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This specification consists of pages i : 
to iv and 1 toll Uulaaivm. 

















This specification consists pf pages 1 
to iv and 1 to 14 ihclusiva. 



Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment. 



















PHOTOGRAPHIC SCALE ONLY 

























Apollo G&N Specification 

PS-1000283 
15 *tay 1963 

Clu* B Releu* 

TERR Ol*-<r(r 


Apollo G&N Specification 

ps -1000283 
15 May 1963 


Apollo G&N Specification 
ps- 1000283 
15 Ray 1963 


PROOTRBtERT SPECIFICATION 

TEMPERATURE ALARM AH) BACKUP CORTROL AMPLIFIER (MA17A-1) 


Record of Rerislona 


Revision 

Letter 

TERR 

No. 

Pages 

Revised 

Approvals 

Date 

MIT 

NASA 






































This specification consists of page 1 to ill and 
1 to $ Inclusive. 


TEMPERATURE ALARM AND BACKUP CONTROL AMPLIFIER (MAlJA-l) 


The purpose of this document is to establish the manufacturing 
and test requirements for procurement. The taperature Alarm and fecfcup 
Control Amplifier (MA17A-1) is Intended for use 1m the Apollo Guidance 
and Navigation Equipment program. 


uJ 

krMNSTRVKLffJHpON LABORATORY 

?//{■/<! 


NASA/MSC APPROVAL 


11 


PROCUREMENT SPECIFICATION 

TOffERATURE ALARM AND BACKUP CONTROL AMPLIFIER (MA17A-1) 


1. SCOPE 

1*1 This specification establishes the requirements for the 

procurement of the Temperature Alarm and Backup Control 

Amplifier (MA17A-1) hereinafter called the amplifier. 

2. APPLICABLE DOCUMENTS 

2.1 The following documents of the issue 1m effect on the date 

of Invitation for bids fern a part of this specification to 
the extent specified herein. 


SPECIFICATIONS 

Military 

MIL-T-27 

MIL-P-116 

MIL-1-16910 

MIL-P-17555 

Apollo G&N 
STANDARDS 
Military 

MIL-STD-810 


CRAVINGS 
Apollo G&N 

1010039 

1010273 

1000283 


Transformers and Inductors 

Preservation, Methods of 

Interference Measurement, Radio, Methods and 
Limits, 14 Kilocycles to 10000 Megacycles 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for Delivery 
of 


Environmental Test Methods for Aerospaoe and 
Ground Equipment . 


Apollo IMU Temperature Control System - Schematic 

2N172A Silicon Power Transistor 

Tbnperature Alana.and Backup Control Amplifisri 
<MA17A-1> 


1 














1 *■ f 

















































Apollo G&.N Specification 
PS-1000284 -A 
15 May 1963 

Class B Release 
TDRR 0 I (0 y 

/ 


Apollo G&N Specification 

PS-1000284 

15 May 1963 


PROCUREMENT SPECIFICATION 
IRIG AND ACCELEROMETER TEMPERATURE 

INDICATING BRIDGE AMPLIFIER (MA16B-1) 



Record of Revisions 


Revisions 

Letter 

TL>rr 

No. 

Pages 

Revised 

Approvals 

DATE 

MIT 

■ -NASA- 

A 

oztfl 

~KeV. "A"replaced 
by Rev. "B* with 
changea. 

k/tl 

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• ftev V tertACeb ar 

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1 


IRIG AND ACCELEROMETER TEMP£R ATURE 
INDICATING BRIDGE AMPLIFIER (K \16B-1) 


— w uie manuiacturing 

and test requirements for procurement. IRIG and Accelerometer Temperature 
Indicating Bridge Amplifier is intended for use in the Apollo Guidance and 
Navigation Equipment program. 


MIT ^ MENTATION L^pb RATORy 






i 


4 

I 

I 


Apollo G&N Specification 

PS-1000284- 

15 May 1963 


PROCUREMENT SPECIFICATION 
IRIG AND ACCELEROMETER TEMPERATURE 
INDICATING BRIDGE AMPLIFIER (MA16B-1) 


1. SCOPE 

1.1 This specification establishes the requirements for the procurement 

of the IRIG and Accelerometer Temperature Indicating Bridge 

Amplifier (MA16B-1) hereinafter called the amplifier. 

2. APPLICABLE DOCUMENTS 

2.1 The following documents of the issue in effect on the date of 
invitation for bids form a part of this specification to the extent 
specified herein. 

SPECIFICATIONS 

Military 

MIL-T-27 Transformers and Inductors 

MIL-P-116 . Preservation, Methods of 

MIL-I-16910 Interference Measurement, Radio Method 

and Limits, 14 Kilocycles to 100 Megacycles 

MIL-P-17555 Electronic and Electrical Equipment and 

Associated Repair Parts, Preparation for 
Delivery of 


STANDARDS 

Military 

MIL-STD-810 Environmental Test Methods for Aerospace 

and Ground Equipment 

DRAWINGS 

Apollo G&N 



This specification consists of pages i to iii and 
1 to 6 inclusive. 


1010039 Apollo IMU Temperature Control - Schematic 

1000283 Apollo IMU Temperature Alarm a;id Backup 

Control Amplifier 

1000284 IRIG and Accelerometer *femperatare Indie a tin 

Bridge Amplifier (MA16B-1) 


f 


ii 


1 

















I tarn I vru _ OEsewtenow _ 

I REPLACES REV A WITH CH 
I K 4 UPGRADED CLASS A 
^ TDRR 




VIEW WITH COVER 


REMOVED 



SECTION A-A 



notes: 

I. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. VAU „ 

^ IDENTIFY USING DRAWING NO, REVISION LETTER, SERIAL NO, / MANUFACTURERS SYMBOL PER MU--STD-I30 
3rENCAP5ULATE WITH EPOXY PER ND 1002036, CURING CYCLE B- 

4. ASSEMBLY TO MEET REQUIREMENTS OF PS 100284. 

5. USE SN60 SOLDER PER QQ-S-571 FOR ALL ELECTRICAL CONNECTIONS - 

Q. USE SN SO SOLDER PER QQ-S-5TI TO SOLDER COVER ASSEMBLY TO CASE 

•777 7 FINISH-VONYL WASH 4 ZINC CHROMATE PRIMER PER MIL-P-C809 TYPE I, PAINT BLACK PER FED-STD-595, NO. 2703S 
\JBL/T/3 TO BE SELECTED PER ATP AOOOZ94- AFTER A/t/T/AL EAUCAPSULAT/OAt 

[raMSE OF VALUES, FROM A* 5 Tf/Rt/ E.49K 0//A4S A A/ STEPS OF EO QA/aRS PER PART AKA. IQI03H 

- lL two resastors may be used ro get Value-Keeded 

It R-f TO BE SELECTED PER ATP AOOOE8+ AFTER AA/aTAAL £f/CAPSi/LAT/oU - 

L RAA/GE OF YALl/E, FROM I7.BK TKRd 30. / KOa/MS /At STEPS OF AOO Oa/MS ^ 

T IZ TWO RESISTORS MAY 3£ itSED TO GET VALUE WEEDED . PER PART Ate* 10/03/1 

Z AO. RSsR/+,R/f ro BE SELECTED PER ATP AOOO&84- PR/OR TO Ea/cAPSUlATAOA/ 

_7 RA/UGE OF VALUES. FROM i7.B/< T/tRit JO.AK OKMS /At STEPS OF AOO O/tARS 

ZZ TWO RESASTORS MAT BE USED TO GET V/tLl/E AtEEDED . PER PART A/O, /O/OJ/t 

tLWHtO/ite RESlSTAAfcE FOR ACCEPTANCE TEST/Atel . 

_ coa/trol h//a/o/Mss / 5 + * /% atews EAot _ere: ;:r— 

X TERAR/a/ALS G f5 AAt0 3j+ „ - 

_ ; bota/ coa/trol WaaIda/Ugs sa/all be AAArcFED W/T/t/Af O*/ OKMS* 

_ fit R/e (EXTERNAL FEEDBACK RES/STOP) TO BE SELECTED PER /ATP AOOOB84- 
RA/tGE OF VALUES , FROM AK T*tRtA 30 K O/tMS AA/ STEPS OF tOO Oa/**S 
7 : : PER PART Kb* A0/03At. OAtLY Oa/e RESASTOR MAY BE USED. 

RESASTOR PitRA/ASA/EO BY YEa/DOR 


WIRING ASSEMBLY 

1001636 


SCHEMATIC 

10016 SO 


RESISTOR 

10IO3U 

SAT 

RESISTOR 

1010311 

SAT 

DIODE 

1010497 

UTR52 

REACTOR ASSEMBLY 

1001638 


REACTOR ASSEMBLY 

1001637 


TRANSFORMER. POWER 

1001549 


PRINTED CIRCUIT ASSEMBLY 

I00IG2G 


CASE ASSEMBLY 

1001548 


COVER ASSEMBLY 

1001547 


PLATE - IDENTIFICATION 

1001543 



REF 

REF 
NOTE IP 
NOTEta" 


LIST OF PARTS AND MATERIALS 

IRIG a ACCEL 
TEMPERATURE 
INDICATING BRIDGE 
AMPLIFIER 


_ 00 WOT 9CMS T 

1000284 HATENIAl: 
r msv into ow 

APPLICATION __ 


Pf/IJ. AATNOVAt OATS 

DSST 


SPACECRAFT CENTEN 
howto* tpcao 
NASA HMMMM NO. 

1000284 

SHEET OF _ 




























































Apollo a ft N Specification Apollo O&N Specification 

PS-1000284-B PS-1000284-B 




ND-1015404 General Specification, Configuration, 

Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment. 




















































3 


i 

•4 

f 




1A 


i 




UNTERPAEi* DRAWING M ACCORDANCE PltM STANDARDS PRESCRIBED BY M'L-D-70327 

2 IDENTIFY USING DRAWING NO, REVISION LETTER, SERIAL NO, / MANUFACTURERS SYMBOL PER MU.-ST0-I3O 

3. ENCAPSULATE WITW EPOXY PER ND 1002036, CURING CYCLE B - -_—. 

4. ASSEMBLY TO MEET REQUIREMENTS OF PS 100284. 

3. SOLDERIN& OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE WITH AWL-STD-4 AO WITH SNSOWAAPR SOLDER PER QQ-S-S7I 
&. SOLDER COVER ASSEMBLY TO CASE PER M/L-S-6B7EA INITN SNSOWAAPR SOLDER PER QQ-S-S7I 
JLPIHJSHl V/NYL INASH PER MIL -C - 1532 a AND ZINC CHROMATE PRIMER PER MIL-P-Q5B5A* 

PAINT BLACK SEMI-GLOSS ENAMEL TT-ES29 CLASS B COLOR 27038 PER FED-STD-595- 
: BLR/3 TO BE SELECTED per ATP 1000234- AFTER INITIAL Ea/caPSiJLATIOW 
RANGE OF YALES** PPQM L5 rHplI 2.4 $KqNmS PER PART NO. 10106$ 4- - 

: - Z TWO PESISTOPS MAY BE MSED TO GET YaLUE. WEEDED . ...Z.'_ 

~ \R+TO BE SELECTED PER ATP 1000234- AFTER INITIAL eWcaPSI/LAT/ oW ““ 

- ■ _Z. PaWge or YALdESj prom !7. ok rWRd so. / koWms __ 

£ JJ .TWO RESISTORS MAY BE USED TO GET YALtfE WEEDED* PER PART NO. 10106$ 4- 

B. RS>A/4 t R/5 TO BE SELECTED PER ATP 1000204 PR/OR TO Eh/cAPSWlAT/oW 

_r: RA/feE or YAUHESj PAQM 17.BK Mud JO.fR OdMS . 

ZZ' TWO RESISTORS MAY BE WSED TO GET MUME WEEDED . PER RAPT WO. 10106 $4- “ZZ... 

TLWnioufG RESISTANCE rap acceptaNce test/Wbi ... 

__ CONTROL M/iNd/MmS 154- ±2%oNmS EACN .I , . 1_ ' - 

^ terminals g/s aNos4+ “ . ; r 

~ \ oorN control w/Wg/Ngs sNall be matcNed witNjN o,/ oNms. 

_ m, M3/EXTERNAL FEEDBACK RESISTOR) TO BE SELECTED PER iATR 1000234- 

z .iw range or yalNes, from ik tnrw 30 r oWms /N steps or too ohms 

7t PER PART WO. 1010311* TWO RESISTOR VALUES SHALL BE SELECTED AND BOTH RAPT NUMBERS AND 
... Z ,Q A S N NUMBERS SHALL BE MARKED OH THE COVER* AS SHOWN* PEA NO 100201$ AND I002l22 T/PEJT CLASS 2 
<3 R7 70 BE SELECTED PEA ATP 1000234 AFTER INITIAL ENCAPSULATION Z . 

__ RANGE OP VALUES* PROM 5K THAU ISK OHMS . . 

“ TWO RESISTORS MAY BE USED TO GET VALUE WEEDED. PEA PART MX 101069* 

I4t INSULATE ELECTRICAL COMPONENTS PROM CASE WITH A .007 GRAY FIBER SWEET PER MIL -X- 69 5A TYPE P 

WITH A MINIMUM DIELECTRIC STRENGTH OP ESO VOLTS PER MIL __ _- 

J5. CENTER IDENTIFICATION PLATE OYER POTTING HOLE - . ;ZZ....„..Z.Z. _ 












































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VIEW WITH COVER 
REMOVED 



K- .203 TYP. 
I BE F. 


6 9 5 6 1 

/O v lT\ lt \ /Ov lT\ 
\3/ V^/ \y\Z/ 

•use with ioiosiC 


10 7 4 3 2 


V/£LW B m B 


_ REVISIONS 

DESCWmON DATE 

' REPLACES REV A WITH CHANGES 

4 upgraded class a r 

TPRR OlfrH Lz 

' revised per tore QS3S4 ^ 

' REVISED PER TPR.E 0S8S9 
' REVISED PER TPRR 06066 /“3/y* 


-SEE NOTE 16 


SECTION A-A 





VIEW C-C 


4-40NC-2A-' 

C C 

T T 

NOTES: 

\JNTERPRET DRAWING Iff ACCORDANCE. IAIITN STANDARDS PRESCRIBED BY M!L-D~70367 

2 IDENTIFY USING DRAWING NO, REVISION LETTER, SERIAL NO, 4 MANUFACTURERS SYMBOL PER IVUL-STD-130 

3. ENCAPSULATE WITH EPOXY PER ND 1002036, CURING CYCLE B _____—.- 

4. ASSEMBLY TO MEET. REQUIREMENTS OF PS 1000284. 

6- solder cover assembly ro case per. mil-s-gbtea with snsowrapr solder per oq-s-57! 

7. FINISH: VINYL WASH P£R M/L-C - /532a AND ZINC CHROMATE PRIMER PER MIL- P-QSB5A* 

7 —. PAINT BLACK SEMI-GLOSS ENAMEL. TT-E-S2$ CLASS 3 COLOR 27036 PER FED-STD- 5^5 

6L/T/3 TO 33 SELECTED PEP ATP 1000234- APTEP iN/TIAL Ea/caFSHlATION 
PANGE OP VALUES, FPQM 1.5K 77/Ptf 6.49K Ot/MS PER PART NO. 1010*9 4* 

~ TWO RESISTORS MAY BE dSED TO GET VALUE NEEDED 

~ \ R+ TO BE SELECTED PEP ATP 1000664- AFTER /NlTIAL Ej/cAPsHlAT/OA( 
range of values, from 17 . bk then so. t koNms 
-i TWO RESISTORS MAYBE tiSED TO GET i/ALifC NEEDED • PER PART NO. 1010694- 

. 47 . RfjRI+jP/f rose SELECTED PER ATP 1000634- PR/OP W eNcAPSJlAT/O f/ 

_r range of yalneSj frqm h.Bk tNrl/ 30 .fR oNms 

ZZ. TWO RESfSTORE MAY BE ifSED TO GET VALUE NEEDED. PER PART NO. IOJ06J4 

!L WtY d ate resistance pop acceptance test/Ngx 
_ . CONTROL VY/No/Ates f54-±2% ONfVtS EACN 

Z TERMINALS 6(5 ANO 34+ 

-t bqtN control WiNdiNgs shall be matched WitNii/ o./ oNms. 

_ B. RtB(EXTERNAL FEEDBACK RESISTOR) TO BE SELECTED PER sATP 1000604- 

range of values, from IK thru 30 k oNms. 

PER PART No. 10103 fU TWO RESISTOR. VALUES SHALL BE SELECTED AND BOTH 
7 DASH NUMBERS SHALL BE MARKED ON THE COYER, AS SHOWN, PER NO 100601 $ AND 1006166 TYPES CLASS 1 

3 R7 TO BE SELECTED PER ATP 1000634 AFTER INITIAL ENCAPSULATION 

-.I RANGE OF VALUES, FROM SK THRU IS KONMS . 

~ TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 101069 4 

f4t INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A .007 GRAY FIBER SHEET PER M/L-Z- 69 SA TYPE P 
WITH A MINIMUM DIELECTRIC STRENGTH OF 250 VOLTS PER MIL 
- 75. CENTER IDENTIFICATION PLATE OYER POTTING HOLE. ! 7._Z. 


5. SOLDERING OF TERMINALS TO BE IN ACCORDANCE WITH MIL-STD-440. ALL 
OTHER ELECTRICAL CONNECTIONS SOLDER PER MIL-S-6872 WITH SN60 
WRAP2 SOLDER PER Q0-S-57I. 

16.TOP DASH NO. IS FOR IRIG BRIDGE IND. AMPL.CONFIGURATION, BOTTOM DASH 
NO. FOR ACCEL BRIDGE IND. AMPL.CONFIGURATION. 


WIRE 

1006711-13 

AWG 30 


13 

GRAY FIBER SHEET 



NOTE 14- 

la 1 

RESISTOR. 

1010694- 

3 AT 

NOTE 13 

// 

WIRING ASSEMBLY 

1001636 


REF 

. 

SCHEMATIC 

IOOI6SO 


REF 


RESISTOR 

1010094- 

SAT 

NOTE 10 

]0j 

RESISTOR 

IOIO<o94- 

SAT 

NOTEfft 

JLj 

DIODE 

1010497 

500 P/V 

3.4-VY 

JU 

REACTOR 

100/540 



7 

REACTOR 

fOOt 5 50 



6 

TRANSFORMER, POWER 

1001549 



5 

PRINTED CIRCUIT ASSEMBLY 

1001626 



4 

CASE ASSEMBLY 

1001548 



3 

COVER ASSEMBLY 

1001547 



2 

PLATE-IDENTIFICATION 

1001543 



1 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS AM IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANOUS 


00 NOT SCALE THIS DRAWING 

1007061 lQ/0039 mnmk: 

NEAT ASSY USED ON 

APPUCATKMI 


M I T 

INDYWUMENTATION L 


LIST OF PARTS AMO MATERIALS 

IRIG a ACCEL 
TEMPERATURE 
INDICATING BRIDGE 
AMPLIFIER 


SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA ORAWINQ NO. 

1000284 

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This specification consists of Pages i to iv and 1 to 1$ inclusive 





















Apollo 0 ft If Specification 
PS-1000284-t 

Class A Release 

TDRR 02266 
15 May 10*3 


PROCUREMENT SPECIFICATION 
FOR 

IRIO AND ACCELEROMETER TEMPERATURE 
INDICATING BRIDGE AMPLIFIER 


Revision 
| Letter 


B 

C 

D 


0 * 


TDRR ' Pa ( 50 s 

No. Revised 


r * ■ , * 


05C1« 


replaces 

Rev .*A* with change# 



Page 2. 



Date 



10 Dec.*63 
? Jan.* 64 


This specification consists of Pages 1 to lv and 1 to 15 Inclusive. 





















Apollo 0 % N Specification 
PS-1000284-B 
5 Sept. 1763 


I RIG AND ACCELEROMETER TEMPERATURE 
INDICATING BRIDGE AMPLIFIER 


The purpose of this document Is to establish the 
manufacturing and test requirements for procurement of the IRIO and 
Accelerometer Temperature Indicating Bridge Amplifier which Is in¬ 
tended for use in the Apollo Guidance and Navigation Equipment pro¬ 


gram. 


























PREPARED BY 





APPROVED BY 


Apollo G & N Specification 
PS-10002°4-C 

^ -Sept • 

26 Sept. 1963 


TITLE 


1^. Y.<£Z 


TITLE 




DATE 

/7(j 


TITLE 


DATE 



















Apollo G ft N Specification 
PS-1000284-B 

v Sept* i9^3 


PROCUREMENT SPECIFICATION 
FOR 

IRIO AND ACCELEROMETER TEMPERATURE 
INDICATING BRIDGE AMPLIFIER 


TABLE OF CONTENTS 


SECTION 

1 

2 

3 

4 

5 

6 


PAGE 

SCOPE. x 

APPLICABLE DOCUMENTS % 

REQUIREMENTS .. # 2 

QUALITY ASSURANCE PROVISIONS .... $ 

PREPARATION FOR DELIVERY ...... 14 

NOTES ......... 


















Apollo O&N Specification 
PS-1000284-C 
5 S ept , 1 ^3 
26 Sent, 196’ 


PROCUREMENT SPECIFICATION 
IRIO AND ACCELEROMETER TEMPERATURE 
INDICATING BRIDGE AMPLIFIER 


1. SCOPE 

1.1 SCOPE. This specification establishes the requirements for the 

procurement of the IRIO and Accelerometer Temperature Indicating 
Bridge Amplifier hereinafter called amplifier. 

2. APPLICABLE DOCUMENTS 


2.1 


The following documents of the issue In effect on the date of in¬ 
vitation for bids form a part of this specification to the extent 
specified herein. 

SPECIFICATIONS 


Military 

MIL-P-116 

MIL-E-17555 

Apollo G ft N 
ND-1002023 

ND-1002059 
ND-1015404 


N£-1002019 


Preservation, Methods of 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of 


Procedure for Serialization of Components, 
Assemblies, etc., for Apollo Guidance and 
Navigation Equipment. 

Qualification Specification, Magnetic 
Amplifiers 

General Specification, Configuration, 
Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use In Spacecraft and Supporting 
Equipment. 

Marking, leneral Specification for 


1 
































Apollo G&N Specification 
PS-1000284-B 
10 D ece mb er 19 ^ 3 
7 January 196A 

STANDARDS 

Federal 

FBD-STD-595 Colors 

Military 

MIL-STD-130 Identification Marking of TJ.S. 

Military Property 

- MIL-STD-202 Test Methods for Electronic and 

Electrical Component Parts 

DRAWINGS 


Apollo G&N 
1000284 

1001540 

1001549 


IRIG and Accelerometer Temperature 
Indicating Bridge Amplifier 

Coil 8c Core Assembly (Reactor 2nd Stage) 

Coil & Core Assembly (Power Transformer) 


1001550 Coll & Core Assembly (Reactor 1st Stage) 

(Cop-.es of Spec-.* _ cations, standards, drawings, and publications 
required by suppliers in connection with specific procurement 
functions should be obtained from the procuring activity or as 
directed by the contracting officer). 

2.2 CONFLICTING REQUIREMENTS. In the event of conflict between the 
requirements of this specification and other specifications and 
drawings cited herein, resolution must be obtained from the MIT 
Apollo Management Office via the purchaser. 


3. REQUIREMENTS 

The requirements of th* oecification are classified Into two 
headings: 

General Requirements which are defined in paragraph 3.2 
and Performance and Product Characteristics which are 
defined in paragraph 3*3 

3*1 DESCRIPTION. The amplifier shall be a magnetic amplifier designed 
to linearly amplify the differential current in the legs of a dc 
resistance bridge. The output of the amplifier shall be 0 to 5 vdc 
(6 vdc maximum) proportional to the IRIG or accelerometer temperature 
for use in telemetry (VCC), and to drive the Temperature Alann and 
Backup Control Amplifier via a logic network. The amplifier shall 
have one external feedback resistor to adjust the gain for the IRIG 
temperature application-and another external feedback resistor to 
adjust the gain for the accelerometer temperature application. 

These two feedback resistor values shall be furnished and marked 
on the amplifier by the supplier. 


2 




















Apollo Q Sc N Specification 
ps-iooo?24-B 

Sep* , 1 ^ >- 

10 Tm c. 106? 


3.2 


3.2.1 


3 . 2.2 


3.2.3 


3.2.4 

3.2.4.1 

3.2.4.2 


GENERAL REQUIREMENTS 

qualification Testing . When specified by the purchaser, a 
representative sample of the amplifiers shall be manufactured 
using the methods and procedures proposed for the production lot. 
These shall be submitted to the NASA Inspector for Qualification 
tests at an activity designated in the contract or by the purchaser. 
These qualification tests are conducted to determine whether or 
not the amplifiers are being produced In compliance with the 
requirements of the contract, specification, and drawings. 

Failure of the amplifiers to meet these requirements may result 
in disqualification of the supplier as determined by NASA or the 
purchaser. 

Further production of the item by the supplier prior to approval 
of the purchaser or the completion of qualification tests shall be 
at tne supplier's risk. Requalification will be reouired at the 
discretion of NASA or the purchaser in the event that, (a) the 
supplier has modified the item, (b) the supplier has Instituted 
a change in the material used or in his processing, and (c) the 
specification requirements for the Item have been amended or re¬ 
vised sufficiently to affect the character of the item. 


The oualification tests will be conducted in accordance with the 
procedure specified in Section 4. 


hequallfication Testing . When specified by the procuring 
activity, the supplier shall submit one or more amolifiers to be 
selected from each oroduction lot by the procuring activity for 
submission to a designateo testing activity to determine com¬ 
pliance of the sample (a) with the requirements of the contract 
specification, and drawings. ' 


yateriais and instruction . The materials used in fabricating the 
amour*ers shall be in strict accordance with the aorlicable 
drawings and specifications referenced herein. Substitute 
materials shall be selected with such qualitv as to ensure that 
the eouioment will meet the requirements of this specification 
and shall be subject to prior approval of the procuring activity. 

Dimensions^ Fini sh, and Marking . The weight, dimensions, 
finloh, and margin*, of the amplifier shall comoly with the 
requirements specified, herein or on the applicable drawings. 

Weight . The weight of the amplifier shall not exceed 2.4 ounces. 


Finish . Finish shall be 16 specified cm the epplloeble drawing* 


3 



















Sp.eifie.tlon 

8e p i < 19^3 
10 Dec. ,1963 

4.3 parking. Marking shall he In; acaord&Aoa with MIL-STD-130 and 
Specification NI>-1002019, and as apssinad on the applicable * 
drawing. 


s 


6 


I® 

’ll 


■^■^4-.' iL -ft. - 

nt ( - r r*5«r f'1y ) 
nicer a ssir.ed in 


acn amplifier identified by General Arrange- 
Drawl ns? shall be identified by a serial 
accordance with Specification*ND-1002023. 


* oncrcansn 1 t 
nr ;•••• mr,l !ss, 

in "*‘rvi / '. , 


JL 


“ h " fabrication and finish of the amplifier. Its 
jra-^embUes. and parts shall be such as to produce 
rcrr. any defect that would affect proper functioning 


7 


Warranty. A warranty shall 
by correction or replacement 
to be defective In material 
(6) months after acceptance. 


provide for the supplier to remedy 
any component or end item found 
or workmanship not later than six. 


The allowability of the cost of any such 
ment shall be determined as provided in 
appropriate contrac* ent 4 tied "Allowable 
Payment , and Inspection and Correction 


correction or replace- 
the clauses of the 
Cos% »lx«d Tee and 
of Defects". 



i ‘ 1 .n is intended to meet 

a 4 1-ast ?C,COC hours of ooera- 
tr® surv-ier's test time of * he completed unit. 



teaspera^ur* 


Th» amplifier design is intended 
l®ast c years, w« * h * ;t operation, 
a f f e r r ! ns i sccen* an®* «t the *■>***■ 


to have a shelf 
t ambient room 
•1 i°r # s plant. 


r eh ny a :: ~ e a n t p ro :-rjc"" 

~ lire me r. * r - r® s t oted to 
'''h G ra^*«''' < '*!c > s rd ^f * 
e ?irn. ' n -1 n «i on c f t h 

ry the currlier as autho 


1HARAC~3hIT rI CS . The following re¬ 
in form ♦ne supplier of specific 
^e goals that were considered in the 
is information shall net be construed 
Azat ion to modify the design. . 


If the design of any part Is not completely specified by the 
contractual documents, the supplier may submit a suggested 
design document for approval which will support these require¬ 
ments. 


If, in the opinion of the supplier, any design or testing 
shall impose undue time delay or expense, he shall so atate. 

In detail. In a counter-proposal, substantiating all contrib¬ 
uting factors when submitting a bid, proposal, or change request 
in connection with this ?peo!^i^a*ion. 


4 





















3.3.1 

3.3.1.1 


3.3.1.2 


3.3.1.3 


3.3.1.4 


3.3.1.4.1 


3.3.1.4.2 


Apollo 3 1 K 3p«0lfloatloo 

& & 8 m y %i ’ 1 9 M * 

10 Dec. *1 >63 

Requests fop chants op deviations to this specification op to 
applicable drawings, specifications, publications, materials, op 
processes specified herein shall be accompanied by written 
Justification. 

Functional Requirements . 

Winding Resistances . DC resistance of the windings shall be as 
specified on Apollo Q ft N Drawing 1000284, 100154©. 1001544. and 
1001550. * 

Dielectric . Strength . The amplifier shall exhibit no evidence of 
breakdown when subjected to a 500V rms voltage. : v 

tnsulatlon Resistance . The Insulation resistance of the amplifier 
shall be lOO megohms minimum. ... 

Performance . Performance of the amplifier shall be as follows* 

M aximum Current Input . Maximum current input shall not exceed 
3o ma under any" conditions. .... 

M aximum Output . Maximum output shall not exceed +6.00 vdc. 


3.3.1.4.3 


3.3.1.4.4 


3.3.1.4.5 


M J . n f n P i> Output . Minimum output shall be between -0.70 vdc and 
+ 0.10 vdc. .... 

D ifferential Balance . When equal currents of 6.00 + 0.12 ma are 
nowing through both input windings, the output shall be 2.5 
+ 0.1 VdC. » V':' .... 

Qaln and Linear ity-Accelerometer Appllcetton. When eaual 6.00 
+ 0.12 ma dc reference currents are fTow'IWg through both Input 
windings and when the current throu^ one winding is then increased 
or decreased as specified In Table I, the output shall be as 
specified in that table. The amplifier shall operate as specified 
after reaching thermal stability with the ambient temperature 
specified in 4.2.1 and again after reaching thermal stability 
with an ambient temperature of 150° *5°F. when the ambient 
temperature is returned to that specified in 4.2.1 and after 
thermal stabilization occurs, the amplifier shall again operate as 
specified. ?, : . ... 


I 


Table I. Accelerometer Application 


Current in one winding 
varied as follows: 


Output voltage 
shall be« 


-46 • 0 M- amp 
-25.0 jul amp 
0.0 

♦23. C jm amp 
+46.0 amp 


0.00 f 0.20 vdc 
1.25 ^ 0.15 vdc 
2.50 T 0.10 vdc 
3.75 ** 0.15 vdc 
5.00 + 0.20 vuc 










3.3.1.4.6 


Apollo 0 ft If Specification 
PS-1000264-$ 

i * 

10 Dec* 1963 

Hippie . Output peak-to-peak ripple shall not exceed 50 mv.(0-10 ka) 


3.3.1.4.7 Output Impedan ce. The output Impedance shall be less than 
l,0o<3 ohms~ r ’ *; . . . 

3*3.1*4.8 Qaln yd Llnearlty-IRIQ Application. When equal 2.00 + 0.04 ma 

dc reference currents are flowing through both input windings and 
when the current through one winding Is varied as specified in 
Table II, the output shall be as specified in that table. The 
amplifier shall operate as specified after reaching thermal 
stability with the ambient temperature specified in 4.2.1 and 
again after reaching thermal stability with an ambient tem¬ 
perature of 1^0° +5°F. When the ambient temperature is returned 
to that specified in 4.2.1 and after thermal stabilization occurs, 
the amplifier shall again operate as specified. 4 ^ 


Table II. IRIO Application 


Current in one winding 
varied as follows: 

Output voltage 
shall be: 

- 92 . 1 * ■ amp 

O.oO + 0.20 vdc 

-46. 0 r amp 

1.25 + 0.15 vdc 

0.0 

2.50 T 0.10 vdc 

♦ 46.3' jlk amp 

3.75 T 0.15 vdc 

♦ 92.10 jjl amp 

5.00 T 0.20 vdc 


3-3.2 Enviro n mental Requirements . The amplifier shall be capable of 

meeting the requirements of Specification NL>- 1002059 . When a 
particular requirement in Specification ND -1002059 Includes the 
amplifier’s capability of operation while being subjected to an 
environment, this shall be construed to mean that an output of 
t 0.15 vdc shall be maintained undef standard operating rr 
conditions as defined in .1.*. 







Apollo 0 ft M Specification 
PS-1000264.1 
5 Sept. 19^3 


3 . 3.3 


3 . 3 . 3.1 


3 . 3 . 3.2 


3 . 3 . 3.3 

3 . 3 . 3.4 


3 - 3 * 3.5 


3 . 3 . 3.6 


3 . 3 . 3.7 


3 . 3 . 3.8 


Design Requirements . 

Tnterchangeabi11ty . Unless otherwise specified, the amplifier 
and its~competentparts shall be physically and functionally 
Interchangeable without selection or fitting. 

Reliability . The amplifier shall be capable of operating a 
minimum of 20,000 consecutive hours without maintenance under 
any combinations of conditions specified herein and shall have 
a maximum failure rate of 0.5 failures per 1,000.000. 

Radio Interference Suppression . The suppression of radio noise 
in'S’Tnterfepence" shall be considered in the design of the amplifier. 

Flammable Mat erials . Materials which may be ignited or cause an 
explosion "shall not be used for construction applications where 
sparking or arcing could cause Ignition. Materials which may 
inadvertently support combustion shall not be used. Flammable 
Impregnating, potting or embedding compounds, when enclosed in 
fire-resistant containers shall be acceptable. 

T oxic Materials . Materials which produce haimful toxic effects 
(luring service usage shall not be used. Where a suitable non- 
toxic material is not available, preventive measures shall be 
provided, subject to the approval of NASA. Materials which 
when ignited, produce toxic substances or vapors shall be avoided 
whenever practicable. 

Unstable Materials . Materials which are unstable or become un¬ 
stable to the extent that they emit or deposit corrosive sub¬ 
stances capable of causing corrosion or producing electrical 
leakage paths within an assembly unde~ possible operating and 
storage conditions shall not be used during manufacture or 
recommended for use during maintenance. 

Co rrosion . Moisture, and Fungus-Resistant Materials . Materials 
shall be selected for noncorrbslve and nonhygroscopie character¬ 
istics and ability to resist the effects of corrosion, moisture 
and fungus. Preference shall be given to materials with inherent 
fungus resistance rather than reliance upon the application of 
surface fungistatic or fungicidal treatments. 

Di ssimilar Metals. The use of dissimilar metals shall be avoided 
whenever practlcable. Magnesium shall not be used except with 
the prior approval of the procuring agency or when so called for 
on the applicable Apollo 0 ft N drawings. 





4. 


4.1 


4.1.1 


4.1.2 


4.2 


4.2.1 


4.2.2 


QUALITY ASSURANCE PROVISIONS 


Apollo 0 & If Specification 
PS-100028A-B 

r 6 O gr t 


10 Dei. IV: 




QKNI5RAL. Unless otherwise specified herein, the supplier is 
responsible for the performance of all inspection requirements 
prior to submission for NASA inspection and acceptance. Except 
as otherwise specified, the supplier may utilize his own facilities 
or any commercial laboratory acceptable to NASA. Inspection 
records of the examinations and tests shall be kept complete and 
available to NASA as specified In the contract or order. The 
supplier shall conform to Class 1 >f Specification ND-1015404. 

Acceptance Tests. These tests shall be accomplished on each 
ampTYfTer being - submitted for acceptance unuer the contract. 
Acceptance test data on each unit accepted must accompany shipment 
to the purchaser. Acceptance tests shall be witnessed by the 
cognizant government inspector, a representative of the purchaser, 
or as the purchaser may direct in the procurement order. These 
tests are detailed in 4.2. Failure of the amplifier to comply 
with these requirements shall result In rejection of the item. 

Qualification and Requalifl cation Tests . Qualification and Re- 
qualifteation tests shall be accomplished at a NASA designated 
activity. These tests, as outlined in 4.3, shall be conducted 
after the award of the contract to determine that the production 
will meet all requirements of this specification. Acceptance shall 
be beseu on no oefects in the amplifier. 


Failure of the amplifier to comply with these requirements shall 
result In the rejection of tht lot or the cessation of production, 
as determlneo by the purchaser. 


ACCEPTANCE TESTS 

Test Conditions. Unless otherwise specified herein, the amplifier 
sK5TT be liubjbeted to tests under the following ambient conditions: 

(a) Temperature: 25 ± 10° C 

(b) Relative Humility: Not more than 9<# 

(c) Barometric Pressure: 28 to 31 inches Hg. 

Test Power. The following electrical inputs, as measured at the 
unit under test, are necessary for testing this Item: 

(n) oo + ?v ms, 3200 + 32 cps, square wave, 1.0 va maximum power. 
The square wave shall Have a rise time of 20 )k seconds maximum 
and a balanced duty cycle within 5-0 percent. 

(b) 19.28+0.1 vdc, 12 ca 

(c) 9,04+0.1 vdc,.4 ®a 


8 












Apollo G&N Specification 
PS-1000284-D 
10 December 19^3 


4.2.3 


4.2.4 

4.2.5 


4.2.6 


4.2.7 
4.2.7«1 
4.2.7.2 


Visual and Mechanical Inspection. A comprehensive inspection 
shall He made 6 f the amplifier To determine the extent of com¬ 
pliance with the requirements of this specification and the 
applicable Apollo Q&N drawing specified in Section 2 and shall 
at least include determination of the followings 

(a) Size, dimension, tolerance, weight, appearance and markings. 

(b) Adequacy of materials, parts, and subassemblies; compliance 
with specific ratings, and conformance to applicable 
specifications. 

(c) Finish, coatings, construction, markings, and nameplates, 
as applicable. 

(d) Wiring, cabling, welding, soldering, color coding, and 
terminals, as applicable. 

(e) Workmanship and cleanup. 

DC Resistance. DC resistance shall be tested by using method 
303 of M1L-T5TD-202 and shall be as specified on Apollo Q&N 
Drawings 1000284, 1001540, 1001549 and 1001550. 

Dielectric Strength. Dielectric strength shall be checked 
by applying a BOcV”rms, °P S voltage between each terminal 

and the case and a 200V rms, 60 cps \10QK source imoedance) 
voltage between the terminals specified in Table ILI. The leakage 
current shall not exceed 1.0 ma. This test shall be conducted 
in accordance with method 301 of MIL-STD-202. 


Table III. Dielectric Strength and Insulation Resistance 


Between Terminals: 

Between Terminals: 

1 and 3 

6 and 3 

1 and 0 

6 and 0 

1 and 8 

3 ana 8 


Insulation Resistance. Insulation resistance shallbe checked 
by applying a 300 v 3 c voltage (current limited to 6 uamp) 
between each terminal and the case and between the teminals 
specified in Table HI. The minimum acceptable resistance shall 
be 100 megohms. This test shall be conducted in accordance 
with method 302 of MIL-STD-202. 

Performance. Performance of the amplifier shall be checked as 
folTow T:—Unless otherwise specified, the amplifier shall be 
connected as specified in test setup shown in Figure 1. 

Maximum Current Input. Adjt a variable resistor R5 to obtain 
the maximum amplTfl er output, (meter M2). The 3200 cps supply 
current shall not exceed 50 ma as indicated on meter Ml. 

Maximum Output. Adjust R5 to its maximum resistance position. 
The output’ voltage (meter M 2 ) shall not exceed +6.00 vdc. 


9 





Apollo G&N Specification 
PS-1000284-D 
10 December 19^3 


4 # 2.7.3 

4.2.7.4 

4. 2 . 7.5 


4.2.7.6 

4.2.7.7 

4.2.7.8 


Minimum Output, Adjust R5 to Its minimum resistance position. 
The output voltage (meter M 2 ) shall be between -0.70 vac and 
+ 0.10 vdc. 

Differential Balance. Adjust R5 to 0 + 10 u volts on M3. 

Voltage at M 2 shall be 2.5 + 0.1 vdc. 

Gain and Linearity-Accelerometer Application. Adjust R5 to the 
values specified in Table TV.. The voltage - at M 2 shall be as 
specified In Table IV.. This test shall be performed three 
times, once in each of the following ambient temperatures in the 
sequence Indicated, after the amplifier and feedback resistor 
(Ro) attain thermal stability in the ambient temperatures 

(a) The temperature specified in 4.2.1 

(b) 150° + 5<>F 

(c) The temperature specified in 4.2.1 

Table 17. Accelerometer Application 


R5 Setting 


38.00 ohms 
49.00 ohms 
60.00 ohms 
71.00 ohms 
82.00 ohms 


Output voltage 
at M2 (vdc) 


0.00+0.20 

1.25+0.15 

2.50'T0.10 

3.75+0.15 

5 . 00 + 0.20 



Hippie. Connect a calibrated oscilloscope in parallel with M2. 

The peak-to-peak ripple shall not exceed 50 mv ( 0-10 kc) for 
any value of R5 specified in Table IV# 

Output Impedance. Adjust R5 for a 4. 0 + 0.1 vdc output at M 2 . 

After closing switch SI, the voltage aT M 2 shall be 2 vc’c minimum. 

Gain and Linearity-IRIG Application. Figure 2 shall be used to 
conduct this test. Adjust R5 to We values specified in Table 
V.. The voltage at M 2 shall be as specified in Table V. This 
test shall be performed three times, once in each of the 
following ambient temperatures, in the sequence indicated, after 
the amplifier and feedback resistor (R 6 ) attain thermal stability • 
In the ambient temperature: 

(a) The temperature specified in 4.2.1 

(b) 150° + 5°F 

(c) The temperature specified in 4.2.1 


10 




































Ap cl1o 5 4 S Specification 

PS-1000284-D 

10 Dec* 1963 


20-2V rms 

A 3200-32 cps 

9.04±0.1 vdc (see 4.2.2.a) 



R1,R2 s 2.OK ±C.l*, matched 
to C.01 ohm at 25°C, 
stable to 15 opm/year, 

T.C. of 5 ppm/oc max* 

R3 = 1 • Q K ±0.01* 

R4 = 2365.3 ohms ±0.0!* 

R5 * 0 to 1.0K decade resis¬ 
tance (G.R. 1432K or equlv.) 

R6 s IRIS Redback Resistor 

(value as marked on amplifier) 
R7 - 25OK ±1.0* 

R8 = 13777 ohms ±0.01* 


Ml sr Thermal Milllameter 

(Weston 622 or equlv.) 

M2 s DC Differential Volt¬ 
meter, C.05 * accuracy 
M3 r DC Mlcrovoltmeter (M.f. 
425A with floated input, 
or equlv.). This meter 
application la highly 
critical and any equiva¬ 
lent meter shall be care¬ 
fully evaluated. 


Figure 2. Test Setup - IRIG Application 








Apollo G&N Specification 
PS-1000284-D 
10 December 15K>3 


TABLE V.I FUG APPLICATION 


R5 Setting 

Output Voltage 
at M2 (vdc) 

767.8 ohms 

064.3 ohms 

565*3 ohms 

470.3 ohms 

37c.3 ohms 

0.00 + 0.20 
1.25 * 0.15 
2.50 + 0.10 
3.75 T 0.15 
5.00 T 0.20 


4.3 QUALIFICATION AND REQUALIFICATION Qualification and re¬ 
qualification tests shall be performed in accordance with Specifi 
cation ND-1002059* When amplifier operation is included as a 
condition in a test in Specification ND-1002059, the amplifier 
shall be operated under standard operating conditions (see 6.1.1) 
The output shall be monitored during operation under standard 
operating conditions and shall be 3*75 + 0.15 vdc at all times. 

4.4 RELIABILITY. The reliability requirements contained in 
Section 3 of this specification are design objectives. Unless 
specifically called for in the procurement contract. It shall 
not be necessary for the supplier to demonstrate his compliance 
with the requirement. The supplier will furnish the purchaser 
or NASA such data as he may have available for establishing the 
current reliability of these units. Additional data shall be 
accumulated to as great a degree as possible from the tests 
specified herein or any other tests the supplier may conduct 
which will tend to support or certify attainment of the 
reliability objectives specified. 


13 














Apollo 3 4 S Specification 
PS-1000284-B 
5 Sept. 1965 


5. PREPARATION *0R DELIVERY 

5.1 PRESERVATION AND PACKAGING. The amplifier shall be pre¬ 
served and packaged In accordance with Specification 
MIL-E-17^5% level B # as specified In the contract or 
purchase order. 

5.1.1 Level S (Halted Military Packaging). Level B packaging 
Is that which will afford adequate protection against 
damage during multiple domestic shipments, handling, and 
covered storage. 

5.1.1.1 Cleaning . Cleaning for Level B preservation and packaging 
shall be In accordance with method C-l of Specification 
KIL-P-116. 

5.1.1 .2 Vnlt Protection. The amplifier shall be Individually 
affor^d unit protection In accordance with method III 
of Specification MIL-P- 116 . In addition, equipment 
packaged for level B protection shall be sealed against 
water and dust by means of suitable wrapping. 

5i2 REPA r R PARTS. Repair parts shall have preservation and 

packaging per the applicable repair parts list an! Its 
packaging supplement. 

5.3 PACK T N3. The ®aulpmert. shell be packed in accordance with 
Specification . M IL-S-r’ crc , level 3. 

5.4 MARKING. In addition to any social marking required by 
the contract or order, the marking of unit, interior 
packager, and exterior shipping containers shall be in 
accordance with level B of Specification MIL-2-1^ 555 . 


6 . NOTES 

6.1 DEFINITIONS 


6.1.1 


For the purposes specified 
. rating conditions shall be 
defined as operation of the arol 1 fler with the Inputs and 
test connections specified In Figure 1 and with R5 (Figure 1) 
set at 71.00 ohms. 



14 
















Apollo 1 + N Coaoi f 1 cat ion 

5° Sept. 1963 


NOTICEI When NASA drawings, specifications, 
and other data are used for any purpose other 
than In connection with a definitely related 
NASA procurement operation, NASA therby Incurs 
no responsibility nor any obligation whatsoever, 
erd the fact that NASA may have formulated, 
fu n1 shed, or in any way supplied the said 
diuwings, specifications, cr other data is 
not to be rgarded by implication or other¬ 
wise as in any manner licensing the holder or 
any person or corporation, or conveying any right 
or permission to manufacture, use or sell any 
patented invention that may in any way be related 
thereto. 


15 


JL 






Av.ollo G ?• V. Specification 

p.;-3.000 <> -E 

Clans A Release 
TDKR OlOf6 
15 May 1063 


PROCUREMENT SPECIFICATION * 

FOR ' v . 

IRIO AND ACCELEROMETER TEMPERATURE v““ 
INDICATINO BRIDGE AMPLIFIER **:■ 


Pn^os 

Revised 


_Anorovala _ . 

“MIT 1 "NAS/T Date 




„ 0 • Rev.^B** replaces’ ///)'> •' ’ ^ J//; C-.. 

CV’w/ Rev."A" with changer. ^ ^ I' 

■ —* — -- ' S, m i <*/) • ' •*. 

o:- - ?:.-r * - 

QC ,—<T- r ?^7 r r ; ' J ,3.*, c 4.% < >. I.J i l 10 >e.*«3 

„, C!5 - lr „- J . ■:<//<. , 4 ? :' V “- ** 

,«« l.B. 11. li ^ *“ >JB 


This specif?cation 


consists of Po?« 1 t° 8nd 1 t0 15 lo ciJ3lve * 














Apollo G&N Specification 
PS-1000264 F 


PROCUREMENT SPECIFICATION 
DUG AND ACCELEROMETER TEMPERATURE 
INDICATING BRIDGE AMPLIFIER 


1. SCOPE 

1.1 SCOPE. This specification establishes the requirements for the procurement of the IRIG 
and Accelerometer Temperature Indicating Bridge Amplifier hereinafter called amplifier. 

1.2 CLASSIFICATION. The requirements for the equipment covered by this specification shall 
be classified as follows: Unless identified by the respective type, all requirements of this 
specification are applicable for all types. 

a. Type I: The requirements for Part Number 1000284-000 shall be designated as Type I . 
in this specification and identified as PS 1000284-000. 

b. Type II: The requirements for Part Number 1000284-011 shall be designated as Type II 
in this specification and identified as PS 1000284-011. 

2. APPLICABLE DOCUMENTS 

2.1 The following documents of the issue in effect on the date of invitation for bids form a part 
of this specification to the extent specified herein. 


SPECIFICATIONS 

Military 

MIL-P-116 Preservation, Methods of 

MIL-E-17555 Electronic and Electrical Equipment and Associated 

Repair Parts, Preparation for Delivery of 


Apollo G & N 

ND-1002023 Procedure for Serialization of Components, Assemblies, 

etc., for Apollo Guidance and Navigation Equipment 

ND-1002059 Qualification Specification, Magnetic Amplifiers 


ND-1015404 General Specification, Configuration, Process and 

Quality Control Requirements for Suppliers of 
High Reliability Articles for Use in Spacecraft 
and Supporting Equipment 


ND-1002019 Marking, General Specification for 


1 











Apollo 9H 3ne: mention 
PS-100028A-I 


4. QUALITY AEEURANCE PR0VI3I0NG 

4 #1 GENERAL. Unless otherwise specified herein, the supplier Is 

responsible for the performance of all Inspection requirements 
prior to submission for NASA inspection anc acceptance. Except 
as otherwise specified, the supplier mav utilize his own facilities 
or an? commercial laboratory acceptable to NASA. Inspection 
reco-cs of the examination 3 and tests shall be kept complete and 
available to NASA as specified in the contract or order. The 
supplier shall conform to Glass 1 of Specification ND-I01p404. 

4)1 Acceptance Tests. These tests shall be accompltshed on each 

ambinTlVrTieliVc^submitted for acceptance unuer the contract. 
Acceptance test aata on each unit accepted must accompany shipment 
to the purchaser. Acceptance tests shall be witnessed by the 
'ogr.’zant government Inspector, a representative of the purchaser, 
or'ai the purchaser may direct In the procurement order. These 
tests are detailed «n 4.2. Failure of the amplifier to comely 
with these requirements shall result in rejection of the Item. 

4 . 1.2 Qualification and Re quo 11 f 1 cation Teats. Qualification ’.n<l Re- 
oufn.TficVt'i'on"T^Ta~l&aTT be Vco'crblTeKed at a NA3A deal gnuted 

' activity. These tests, a? outlined In 4.1, shall be conducted 
after the award of the contract to determine that the prediction 
will meet nil requirement? of this specification. Acceptance shall 
be based on no defects- In the amplifier. 

Failure of the amplifier to cornel ' with these requirements shall 
result In the reflection of the lot or the cessation of production, 
as determined by the purchn 3 er. 

4.2 ACCEPTANCE TESTS 

4 . 2.1 Test Conditions* Unless otherw’.se specified herein, the amplifier 
sTuT! Subjected to tests under the following ambient conditions! 

(a) Temperature: ^ ® 

(b) Relative Humidity: Not more then 90£ 

(o) Barometric Pressure: to 31 inches Hg. 

4 . 2.2 Teat Power. The following electrical «nputs, as measured at the 
unit under teat, are necessary for testing this item: 

* (a) Type I, 20 ± 2V rms, or Type 11,21 ± 3V rm®, 3200 ± 32 epe, square wave, 

1 ,0 va maximum power. The square wave shall have a rise time of 20 p seconds 
maximum and a balanced duty cycle within 5.0 percent. 

(b) ld.;:.-o+ 0 ,l vde, 12 ma 

(c ) h.O**’ J-0. 1 vdo, 4 ms 








Apollo 3 A F Speciflcatlo" 

o $ .i r>or oq 4 . p 


20 ± 2 V rms (Type I) 
21*3V rms (Type II) 
3200*32 cpe 

10.? n -0.1 vdc (see 



R1,R2 s 1.5K-0.I*. etched 
to C.01 ohn at ?5°C, 
stable to 15 ppa//ear, 

?.C. of 5 ppa/°C max, 

R3 s 1.5K XO.OK 
R4 r 1.56K *0.01* 

R5 * 0 to 100 ohm decade resis¬ 
tance (G.R. 1432K or equiv) 

R6 * Accel, feedback Resistor 

(value as marked on amplifier) 
R7 r 260K -l.ct 
R5 r 1.OK -1. 0 < 

R9 = 4162 ohms -0.C1* 


Ml z Thermal Mil 1la^meter 

(Weston 6° 7 or equiv.) 

M? s DC Differential Volt¬ 
meter, aecuracy 

M3 3 DC Microvoltmeter (H.P. 
425A with floated Input, 
or eouiv.). This meter 
application is highly 
critical and any equiva¬ 
lent meter shall be care¬ 
fully evaluated. 


v» r.ure 1, Test Setup - Accelerometer Application 


11 







Rl f R2 s 2.0K 
to C 
stab 

r* 

B3 = l.flx’ir 
R4 s ?J6S.3 
R5 * o to 1. 

tance ( 
R6 - IRJ3 *e 
(value 

R? -* 2 C 0K -1 


ched 
?S°C f 
m/year t 
C max. 


esls- 
or equiv.) 
star 

in amplifier) 










Apollo G A *< Eoec ’ f! cat *cn 
PS-10002 8 A -G 

Class A Re 1 ease 
Tl'HR 01 ?66 
1- Vs/; -jVt 


PROCUREMENT SPECIFICATION 
FOR 

IRIG AND ACCELEROMETER TEMPERATURE 
INDICATING BRIDGE AMPLIFIER 


Revivor* TDHR 

letter No. 


Pages 

Revised 


J 

MIT 


orovnls 
~.f.NASA 


Date 


3 




T} 


P 


F 

G 


cy 


O c l-3 • 

o r a~ 

20719 

20752 


replaces * 

Rev." a" with changer 

f n.’.'tc "* 'i *“ ^ ♦ * * 

* ' w * * * • I t *■ I ■ 




io.ii.i5 A.i if 


1.8,11,12 
8 , 9 


i/A •; 

WK 

WK 


1 



JB 

WJR 


// 


10 Dec.^3 

7 r an. # 64 
7/8/65 
7/13/65 


This specification consists of Pages 1 to iv and 1 to 15 inclusive. 


1 


J 





XI 


Apollo ” & N 
Pf-1000284- G 


4. DUALITY ASSURANCE PROVISIONS 

4.1 GENERAL. Unless otherwise specified herein, the supplier 1 - 
responsible for the performance of all Inspection requirements 
prior to submission for NASA Inspection ana acceptance. Except 

as otherwise specified, the supplier may utilize his own fa»*1 11 ties 
or any commercial laboratory acceptable to NASA. Inspection 
records of the examinations and tests shall be kept complete ana 
available to NASA as sped flea In the contract or order. The 
supplier shall conform to Class 1 of Specification ND-101 *3404. 

4.1.1 Acceptance Tests. These tests 3hall be accomplished on each 
ampTHTer"T^TmTsubmltted for acceptance uraor the contract. 
Acceptance test data on each unit accepted must accompany shipment 
to the purchaser. Acceptance tests shall be witnessed by the 
’orpitzant government inspector, a representative of the purchaser, 
or as the purchaser may direct In the procurement order. These 
tests are detailed in 4.2. Failure of the amplifier to comply 
with these requirements shall result in rejection of the Hern. 

4.1.2 Qualification and Requalificatlon_Tests. Qualification and Re- 
uunTi'fTcat 1 on uesTs shall be* aecorrpITsTi’ed at a NASA deslTnated 
actlvltv. These tests, as outlined in 4.}, shall be conuuex-u 
after the awara of the contract to Determine that the pron iotLon 
will meet all requirements of this specification. Acceptance shall 
be based on no defects in the amrlifto*’. 

Failure of the amplifier t > comply with these requirements shall 
result in the rejection of the lot or the cessation ot product ion. 
as determined by the purchaser. 

4.2 ACCEPTANCE TESTS 

4.2.1 Test Conditions. Unless otherwise specified herein, the nmol 1 Tier 

■sHIiTi f&Jacted to tests under the following ambient conn itions- 

(a) Temperature: 25 + 10° C 

(b) Relative Humidity: Not more than Q0$ 

(c ) Barometric Pressure : 28 to 32 inches of Hg. 

(d) The amplifier shall be mounted on a 100 sq inch, 1/8 inch thick 
aluminum heatsink or equivalent. 

4.2.2 Test Power. The following electrical inputs, as measured at the unit under 

test, are necessary for testing this item: * 

(a) Type I, 20±2V rms, or Type II, 21±3V rms, 3200*32 cps, square wave 1.0 va 
maximum power. The square wave shall have a rise time of 20 p seconds maximum 
and a balanced duty cycle within 5.0 percent. 

(b) 19.28*0.1 vdc, 12 ma 

(c) 9.04*0.1 vdc, 4 ma 






9 


Apollo G&N SDeciflcation 
PS-1000284-G 
10 December 19^3 


4.2.3 


4.2.4 

4.2.5 


4.2.6 


4.2.7 

4.2.7.1 

4.2.7.2 


Visual and Mechanical Inspection. A comprehensive inspection 
shall be made of the amplifier to determine the extent of com¬ 
pliance with the requirements of this specification and the 
applicable Apollo G&N drawing specified in Section 2 and shall 
at least include determination of the followings 

(a) Size, dimension, tolerance, weight, appearance and markings. 

(b) Adequacy of materials, parts, and subassemblies; compliance 
with specific ratings, and conformance to applicable 
specifications. 

(c) Finish, coatings, construction, markings, and nameplates, 
as applicable. 

(d) Wiring, cabling, welding, soldering, color coding, and 
terminals, as applicable. 

(e) Workmanship and cleanup. 

DC Resistance. DC resistance shall be tested by using method 
303 of MIL-STD-202 and shall be as specified on Apollo G&N 
Drawings 1000284, 1001540, 1001549 and 1001550. 

Dielectric Strength. Dielectric strength shall be checked 
by applying a fjOoV’rms, 60 cps voltage between each terminal 
and the case and a 200V rms, 65 cos (100K source imoedance) 
voltage between the terminals specified in Table III. The leakage 
current shall not exceed 1.0 ma. This test shall be conducted 
in accordance with method 301 of MIL-STD-202. 

Table III. Dielectric Strength and Insulation Resistance 


Between Terminals: 

Between Terminals: 

1 and 3 

6 and 3 

1 and o 

6 and 8 

1 and 8 

3 and 8 


Insulation Resistance. Insulation resistance shall^be checked 
by applying a Z5U vac voltage (current limited to 6 uamp) 
between each terminal and the case and between the terminals 
specified in Table III. The minimum acceptable resistance shall 
be 100 megohms. This test shall be conducted In accordance 
with method 302 of MIL-STD-202. 

Performance. Performance of the amplifier shall be checked as 
follows. Unless otherwise specified, the amplifier shall be 
connected as specified in the test setup shown In Figure 1. 

Maximum Current Input. Adjust variable resistor R5 to obtain 
the maximum amplTfler output (meter M2). The 3200 cps supply 
current shall not exceed 50 ma as indicated on meter Ml. 

Maximum Outout. Adjust R5 to its maximum resistance position. 
The output""voTtage (meter M2) shall not exceed +6.00 vac. 


9 








































Apollo GAN Specification 

PS-1000284 

15 May 1963 

Class B Release 

TDRR 0 I XU (0 


PROCUREMENT SPECIFICATION 
IRIG AND ACCELEROMETER TEMPERATURE 

INDICATING BRIDGE AMPLIFIER (MA16B-I) 


Record of Revisions 


Revisions 

- TDRIT" 

No. 

Pages 

Approvals 1 

DATE 

Revised 

- MIT 

NASA 














— 

. 





-H 

1 










.L 







Apollo GAN Specification 

PS-1000284 

15 May 1963 


IRIG AND ACCELEROMETER TEMPER ATURE to* 

INDICATING BRIDGE AMPLIFIER A16B-1) j 


The purpose of this document is to establish the manufacturing 
and test requirements for procurement. IRIG and Accelerometer Temperature 
Indicating Bridge Amplifier is intended for use in the Apollo Guidance and 
Navigation Equipment program. 

i 

S 



Apollo GAN Specification 

PS-1000284 

15 May 1963 


PROCUREMENT SPECIFICATION 
IRIG AND ACCELEROMETER TEMPERATURE 
INDICATING BRIDGE AMPLIFIER (MA16B-1) 


1. SCOPE 

1.1 This specification establishes the requirements for the procurement 

of the IRIG and Accelerometer Temperature Indicating Bridge 

Amplifier (MA16B-1) hereinafter called the amplifier. 

2. APPLICABLE DOCUMENTS 

2.1 The following documents of the issue in effect on the date of 
invitation for bids form a part of this specification to the extent 
specified herein. 

SPECIFICATIONS 

Military 

MIL-T-27 Transformers and Inductors 

MIL-P-116 , Preservation, Methods of 

MIL-I-16910 Interference Measurement, Radio Method 

and Limits, 14 Kilocycles to 100 Megacycles 

^Jk-P-17555 Electronic and Electrical Equipment and 

Associated Repair Parts, Preparation for 
Delivery of 


STANDARDS 

Military 

MIL-STD-810 

DRAWINGS 

Apollo GAN 

1010039 

1000283 

1000284 


Environmental Test Methods for Aerospace 
and Ground Equipment 


Apollo IMU Temperature Control - Schematic 

Apollo IMU Temperature Alarm and Backup 
Control Amplifier 

IRIG and Accelerometer 'femperature Indicating 
Bridge Amplifier (MA16B-1) 


This specification consists of pages i to iii and I .1 

} to 6 inclusive. i H \ 

i 

















^wpntmrmifaC 


ifi'-js.. 

r»f | 1 

if i 


C i ! 

it 

6 f 


r t* ©— 

X> 9 
IDo 

-^O —•* 
• #n i 


L 


IOO I 

eLJ 


£(?. SPACES AT ||* £ ^ 
2/ON-CUMULATIVE 


5 83 0001 ffil ”» i "» [ 


REVISIONS 


DATE I APPROVAL 


fa/A RtPLAaa 'ey . 
1?eV 8 with 

t. O^T ^ 

UJ/l 


39 



©->W/| BOV t toy. RMS 

• 3200 CPS - 
-»Lol ^ave z 



-.030 DIA. WELDA&LE 
±.OOt 
.7R£Q>D 


4-40VC-2/J 

C7?£5 Mrs sruo 

2. REQ>D 


FOR DETAILED specifications see 

PROCUREMENT SPECIFICATION 1000235 


FOR INFORMATION ONLY 

CLASS B RELEASE TOR Na. a/X&iT _ DATE 


QTY. 

NOMENCLATURE 

PART OR 


MATERIAL 

FINOl 

REQO. 

OR DESCRIPTION 

IDENTIFYING NO. 

StLvIiIUR 1IVR 

OR NOTES 

iD 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 








DO NOT SCALE THIS DRAWING 



MATERIAL: 

NEXT ASSY 

USED ON 


| APPLICATION 



LIST OF PARTS AND MATERIALS 


M I T 

INSTRUMENTATION LAS 

CONTRACT 


NAS 9153 


ARRWOVEO 
CHECKED I A,t Ml t 


LIV K \f-lM 


w 


( sc 

. rt{M 

MIT/IL APPROVAL I DATE 


TEMPERATURE 
AMPLIFIER . 


CONTROL 


SCALE 




UNIT WT. 


CODE IDENT. 


.. " "MIT .. . 

INSTRUM ENTATION 
LABORATORY 

Camdkidoe. MA—■ 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1000285 


SHEET 


OF 




1 


% 




' ? 
I.-. t 


S3*-‘ 


T1 

. fe 


r 


■»»**>>> 


ft K 


B- i 

*i ■ * 


I- “I 

. . -i 
• • t 

















































Apollo G I I Specification 
PS-1000285-^ 

15 May 1963 
Class B Release 
TDRR O l X C# ^ 



PROCUREMENT SPECIFICATION 

FOR . j. 

TEMPERATURE CONTROL AMPLIFIER (PA36A-1) J 

h 

* 

t 


Record of Revisions 



This specification consists of Page 1 to iii and 
1 to 5 inclusive* 


R£PLA££i> SY REV."8" mti CHAMPS. 




Apollo G & N Spe cification 

PS-1000285 

15 May 1963 


PROCUREMENT SPECIFICATION 
TEMPERATURE CONTROL AMPLIFIER (PA36A-1) 


1. SCOPE 

1.1 This specification establishes the requirements for the procurement 
of the Temperature Control Amplifier (PA36A-1), hereinafter called the 
amplifier. 

2. APPLICABLE DOCUMENTS 

2.1 The following documents of the issue in effect on the date of invitation 
for bids form a part of this specification to the extent specified herein. 

SPECIFICATIONS 

Military 

MIL-T-27 Transformers and Inductors 

MIL-P-116 Preservation, Methods of 

MIL-I-16910 Interference Measurement, Radio, 

Methods and Limits, 14 Kilocycles to 
1000 Megacycles 

MIL-P-17555 Electronic and Electrical Equipment 

and Associated Repair Parts, Prepara¬ 
tion for Delivery of 

Apollo G & N General Specification, Configuration, . 

ND-1015404 General Specification, Configuration, 

Process and Quality Control Requirements 
for Suppliers of High Reliabili y Articles 
for Use in Spacecraft and Supporting 
Equipment 


11 


1 



































I INTERPRET DRAWING IN ACCORDANCE WITH MIL-0-70327. 

Z.F2 TO BE SELECTED PCX ATP WOO 235 AFTER 
v _ /N/T/AL ENCAPSULATION* RANGE OF VALUES, FPOM " 

. 40.2K TNPU IE/ KOUMS tN STEPS OF IK ONMS. TWO PES/STOPS MPT 

BE USED TO GET VALUE DEEDED , , „ , . 

, PEP PAPT So. 101031/(UP TO IOOKoNms) 4 PAPT AD. I0I03G4 (ABO/E IQOK OHMS) 

3 . Identify us/Ng drawing No., reV/s/oN letter^ sep/al no. and 

MANUFACTURERS SYMBOL.. PEP M/L *?TD m /30 

4. ENCAPSULATE Pf/Tti EPOXY PEP ED /00S03G, CURING CYCLE B 
f . ASSEMBLY TO MEET ALL PEQU/PEMCNTS OP PS 1000ZB* 

#. USE SNGO SOLDEP PEP QQ-S- 571 POP ALL ELECTP/CAL CONNECTIONS 

USE SNSO SOLDEP PEP Q<?-3-57/ TO SOLDEP CO/EP ASSEMBLY TO CASE 

7. mihdiiJg rcsista&e for ACcerrAttce rcsnfa " 

__ _ CO NT POL WINDING 1}5 QNMS E £5 ONMS 

TERMINAL 3 4 + 

e. F/N/sUt VINYL wasN aNd z/Nc c/Zpqmate pp/mep : 

PEP MIL-P-6689 types ..'. 


% P7 TO BE SELECTED PEP ATP 1000285 PP/OP TO ENCAPSULATION. 

PAAfeE OF VALUES, FROM 15 K THAN £4,9 K ONMS /N STEPS OF /00 OHMS 
! TWO RES!STOPS MAY BE USED TO GET VALUE NEEDED . PEP PAPT No. / 0 / 0 3N 
ML PG TO BE SELECTED PEP ATP /000395 AFTEP iN/T/AL E/ZcaPsUlAT/wZ 

paNge of Values, fpom isk tNpu 24 •. 9 * ohms /N steps of zoo ohms 
: TWO PES/STOPS MAY BE i/SEO TO GET VALUE NEEDED. PEP PAPT No. B/03/1 
/L P/0 TO BE SELECTED PEP ATP /000BBS AFTEP /N/T/AL ENCAPSULAT/oN 
PANgE of VALUES , FPOM /OK TNpU 24. 9* OHMS /N STEFS OF ZOO ONMS 
TWO PES/STOPS MAY SE NSED TO GET VALUE NEEDED. PEP PAPT No. / 0/03// 
/£. P/3 TO BE SELECTED PEP ATP 1000295 AFTEP SN/T/AL ENCAPSULATION 
RANGE OF VALUESi FPOM £K TNRU BK O/ZmS /N STEPS OF /00 ONMS 
TWO PES/STOPS MAY BE USED TO GEr VALUE NEEDED . PEP PAPT NO. /0J03// 
/X P/4 TO BE SELECTED PEP ATP IOOO&95 PP/OP TO eNCAPsUlAT/oU 
PANGE OF VALUES , FPOM / ONM TNpU Z0 ONMS /N STEPS OF /OHM 
TWO PES/STOPS MAY BE USED TO GET VALUE NEEDED. PEP PAPT NO. 10/0604 


SCUEMAT/C _ 

wiring assembly 


PES/STOP 
PES /STOP 
PESisrop 
CAPAC/TOP 

DIODE _ 

RESISTOR 

RESISTOR 

TRANSFORMER 

REACTOR _ 

REACTOR _ 

REACTOR ASSY 


1001533 
‘ 100/535 


101031 / 

’ / 0 / 03 // 

’ 10 / 031 / 

‘ / 0 IQ 693-3 
10/0497 
~ 1010311 
m tQIO3//,/0JO36i 
’ 1001532 
" 1001531 
" 1001530 
’ 1001528 


SA T 
SAT 
SAT 
140 UF 
UTR5& 
SAT 
SAT 


NOTE \Z f5 
NOTE II 1 4 
NOTES >3 


PRINTED-CIRCUIT ASS'Y 100t5 4 1 

CASE ASSY _ 1001537 

COVER ASSY _ 1001534 

PLATE-IDENTIFICATION 1001543 


LIST OF PARTS AND MATERIALS 

TEMPERATURE l _ 

CONTROL _ 

I AMPLIFIER 
ASSEMBLY 


INSTRUMENT ATION 
LABORATORY 


SPACECRAFT CENTER 
HOUtTON TPw 
NMA 0 MW MW NO. 

1000285 










































































##i m\m**m*&*§ \***»*®) m- on 












zone 1 vrm 


o REPLACES REV A w/rW 

cnaNges / upgraded 

CLASS A TOR A C5&° %aen\ Ujtf. 
— REVISED PER TDRR 0*339 IajE 



VIEW WITH \ 

COVER REMOVED \ />/*' 
\ /€ 



5ECT/ON A A 


—J HR—.203 TYP 
• REF 






1.23 t 
MAX .562 
I REF 



VIEW B-B 


VIEWC-C 


4-40NC-2A 

REF 


notes: - i 

I, INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS - ' * 

PRESCRIBED BY MIL-D-70327, 

Z.R2 TO BE SELECTED PER ATP 4000BBS AFTER 
v _ /N/T/AL CNCAPSULAT/ON. RANGE OF VALUES , PROM r 

- 40.2K rNAU /2i NONMS lN STEPS OF / KONMS. TWO AES/STOPS MAT 

BE USED TO GET VALUE NEEDED 

PEA PAAT /to* f0/0694 , 

~ 3 IDENTIFY USING DRAW/NCit No. y RE\t/S/0N LETTER % SEA/AL AND . 

^MANUFACTURERS SYMBOL. PEA MIL-STD -fBO 

4. ENCAPSULATE W/rN EPOXY PEA A/D /0OBOS6, CURING CYCLE B - - ■ 

f . ASSEMBLY TO MEET ALL REQUIREMENTS OF ' PS /0002B5, 

o 6. SOLDERING OF ELECTRfCAL CONNECTIONS TO BE IN ACCORDANCE WITH 

MU--STD- 440 WITH SN60 WARP2 SOLDER PER 00-S-57I. ' ** _ , 

7. Kim/ttG resistance for AcceRrAtfcc resrn/a 

__ 1 CONTROL WINDING 1)5 QNMS CBS QNMS -~ -- 

TERMINAL 3 4 4- 

i. FINISH:VINYL WASH PER MIL-C-15328 AND IINC CHROMATE PRIMER PER MIL-P-8585A, 
PAINT BLACK SEMI-GLOSS ENAMEL TT-E-629 CLASS B COLOR 27038 PER FED-8TD-595. 


16. INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A.007 GRAY FIBER SHEET PER 
MIL-I-695A TYPE F WITH A MINIMUM DIELECTRIC STRENGTH OF 250 VOLTS PER MIL. 

IZ SOLDER COVER ASSEMBLY TO CASE PER MIL-S-6872A WITH SN50 WARP2 
SOLDER PER Q0-S-57I. 

1 R7 TO BE SELECTED PEA ATP fOOO&BS PA/OR TO eNcAPSULAT/ON. 

AAAtGE OF VALUES, FROM 15 R TNR/J 24.JK ONMS /N STEFS OF /00 QNMS 
7:| TWO RESISTORS MAY BE USED TO GET VALUE NEEDED . PER PART No. /0/0694 

ML AG TO BE SELECTED PEA ATP /O00285 AFTER /N/T/AL eNcaFSNl AT/aN' 
range of values, from /§* tNpN 24.9nonms /Nsteps of /oooums 
r TWO RESISTORS MAY BE NSCO TO GET VALUE NEEDED . PER PART No. 10/0694 
lL RIO TO BE SELECTED PER ATP 1000285 AFTER /N/T/AL ENCAFSUlAT/oN 
range OF VALUES . FROM AON TURN 24. 9* ONMS /N STEPS OF 100 ONMS 
7 TWO RESISTORS MAY SE //SCO TO GET VALUE NEEDED. PER PART No. / 0/0694 
IB. RIB TO ME SELECTED PER ATP 1000285 AFTER fN/T/AL eNcaPSULAT/oN 
RANGE OP VALUES } PROM 2K TNRU 8K QNMS, iN. STEPS OP /00 ONMS 
TWO RES/ST0RS MAY BE USED TO GET VAlNe NEEDED. PEA PART NO. /0/0694 
1$. RI4 TO SE SELECTED PER ATP /Q00&85 PR/OA TO ENCAPsUlAT/oN 
range OP VALUES , FROM I ONm TNrU /O ONMS /N STEPS OF / 0NM 
TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART/NX /Q/0G04- 

14. R3 TO BE SELECTED PER ATP 1000285 PRIOR TO ENCAPSULATION RANGE OF 

VALUES, FROM 300K THRU I MEGOHM TWO RESISTORS MAY BE USE0 TO GET 1“ 

* 1 VALUE NEEDED PER PART NO. 1010693. - 

|D. Ct TP BE SELECTED PER ATP 1000285 PRIOR TO ENCAPSULATION RANGE OF- 

VALUES FROM 30 THRU I40UF PER PART NO. I0Q6789. _ 

15. CENTER IDENTIFICATION PLATE OVER . . _ 

POTTING HOLE. :Y:\ : :* K _ 


GRAY FIBER SHEET _ 

SCNEMA T/C _ 1001533 

Wiring assembly too/535 

RESISTOR _ 1010693 

RESISTOR _ 1010604 

RESISTOR _ 1010694 

RESISTOR _ 1010694 

RESISTOR 1010694 

CAPACITOR _ 1006789 

DIODE _ 10104 9 7 

RESISTOR _ 1010694 

RESISTOR _ 1010694 

TRANSFORMER _ 1001532 

REACTOR _ 1001531 

REACTOR _ 1001530 

REACTOR ASSY _ 1001528 

PRINTED-CIACD/T ASS'Y 1001541 

CASE ASSY _ 1001537 

COVER ASSY _ 1001534 

PLATE-IDENTIFICATION_1001543 . 


LIST OF PARTS ANO MATERIALS 
TEMPERATURE 7 _ 

~ control 

ampl/f/er z _: r _ 
~ assembly s:::: 


SAT 

NOTE 14 

17 

SAT 

NOTE 13 1 

16 

SA T 

NOTE 12 

15 

SAT 

NOTE II 

1 4 

SAT 

NOTE ) 

13 

SAT 

NOTE 15 

12 

500PIV 

3.4 W 

II 

SAT 

NOTE 10 

•0 

SAT 

NOTE 2 

9 


□ 


1007056 1010039 

NEXT AMY UKD ON 


SPACECRAFT CENTER 
HOP I TON TEXAS 
•MSA O NA A WN Q NO. 

1000285 


MTUPTWl 





































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6 


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Ken -aces /ret/ a w/rU 

CHANGES / UPGRADED 
CLASS A rorn c 


REVISED PER TDRR OSM 

REVISED PER TDRR 11648 



O , (“7 s 

-71V // > 


•® ^ fr 

[a o oo! h>®\©. 


VIEW WITH \ 

COVER REMOVED \ /JaT 
V 16 





Section A A 


-hJ| h* .203 TYP 






.22 ~T 

MAX .562 
1 REF 



VIEW B-B 


VIEWC-C 


4-40NC-2A 

REF 


i INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327, 

2; R2 TO BE SELECTED PEA ATP (000285 AFTER 
INITIAL ENCAPSULATION. RANGE OF VALUES , FROM 
40.2K n/RU (Si < OHMS /N STEPS OF tKONMS. WO RESISTORS MAY' 
EE USED TO GET VALUE NEEDED 
PER PART Vo. (0/0694 

3 „ Identify us/Ng draw/Ng a/o., reU/s/oN letter t serial a/0, and 

MANUFACTURERS SYMBOL. PER MIL-STD-130 
4 . ENCAPSULATE W/tN EPOXY PER NO (00203G y curing CYCLE B 


9. ASSEMBLY TO MEET ALL REQUIREMENTS OF PS /000285 


6. SOLDERING OF TERMINALS TO BE IN ACCORDANCE WITH MIL-STD-440. ALL OTHER 

ELECTRICAL CONNECTIONS, SOLDER PER MiL-S-6872 WITH SN6C WRAP2 SOLDER PER 
QQ-S-571. , , 

7. WHQttlG RESISTANCE FOR ACCEPTANCE TESTING 

CONTROL WINDING !J5 ONMS £ 25 ONMS 
TERMINAL 3 4 + 

8. FINISH: VINYL WASH PER MIL-C-15328 AND 2INC CHROMATE PRIMER PER MIL-P-8585A, 
PAINT BLACK SEMI-GLOSS ENAMEL TT-E-529 CLASS B COLOR 27038 PER FED-STD-595. 


16. INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A .007 GRAY FIBER SHEET PER 
MIL-I-695A TYPE F WITH A MINIMUM DIELECTRIC STRENGTH OF 250 VOLTS PER MIL. 

17 SOLDER COVER ASSEMBLY TO CASE PER MIL-S-6872A WITH SN50 WRAP2 
SOLDER PER QQ-S-571. 

% R7 TO BE SELECTED PER ATP (000285 PRIOR TO eNcAPSUlAT/Oa/. 

RANGE OF VALUES, FROM (SR TNRN 24.JH ONMS (N STEPS OF (00 ONMS 
TIRO RESISTORS MAY 8E USED TO GET VALUE NEEDED. PER PART No. (0(0694 
KJ. RG TO BE SELECTED PER ATP /000285 AFTER fW/T/AL eNcAPsUl AT/0*/ 
range of Values, from is* tNru 24 . 91 c onms /N steps of /oo onms 
mo RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART No. (0(0694 
(/. RIO TO BE SELECTED PER ATP (000238 AFTER (NlTIAL ENCAPSULAT/oN 
range OF VALUES t FROM (OK TNrU 24. 9* ONMS (N STEPS OF (00 ONMS 
• TtNO RESISTORS MAY BE i/SEO TO GET VALUE NEEDED. PER PART Nt. / 0/0694 

12. If 13 TO BE SELECTED PER ATP 1000235 AFTER IN/T/AL ENCAPSULATION 
RANGE OF VALUES } FROM 2K TNRU &K ONMS (N STEPS OF (00 ONMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. / 0(0694 

13. R!4 TO BE SELECTED PER ATP (000285 PRIOR TO ENCAPSULATION 
raNgc of values , from ( oNm tNru fo oNms (N steps of (oNm 

TWO RESISTORS MAY BE i/SED TO GET VALUE NEEDED. PER PART //o. 10(060+ * 

14 . R3 TO BE SELECTED PER ATP 1000285 PRIOR TO ENCAPSULATION RANGE OF 

VALUES, FROM 300K THRU I MEGOHM TWO RESISTORS MAY BE USED TO GET --— 

VALUE NEEDED PER PART NO. 1010693. -— 

16. Cl TO BE SELECTED PER ATP 1000285 PRIOR TO ENCAPSULATION RANGE OF__ 

VALUES FROM 30 THRU I40UF PER PART NO. 1006789._" MCT, °^ 

18. CENTER IDENTIFICATION PLATE OVER _ 

POTTING HOLE. ' _ oo not 

1007056 1010039 

NUT ASST USE0 ON 


WIRE 

1006711-13 

AWG 30 

1 

19 

o 

GRAY FIBER SHEET 



NOTE 16 

•9 


scnemat/c 

1001533 


REF 



Wiring assembly 

1001535 


REP 


in 

CO 

RESISTOR 

1010693 

SAT 

NOTE 14 

17 

RESISTOR 

1010604 

SAT 

NOTE 13 

16 

0J 

RES 1ST OR 

1010694 

SA T 

NOTE f& 

15 

O 

o 

o 

RESISTOR 

10/0694 

SAT 

NOTE II 

14 

RESISTOR 

1010694 

SAT 

NOTE 9 

13 

CAPACITOR 

1006789 

SAT 

NOTE 15 

12 


DIODE 

10104-97 

500PIV 

3.4 W 

II 


RESISTOR 

1010694 

SAT 

NOTE 10 

10 


RESISTOR 

1010694 

SAT 

NOTE 2 

9 


TRANSFORMER 

1001532 

• 


8 


REACTOR 

1001531 



7 

h* 

REACTOR 

1001530 



6 


REACTOR ASSY 

1001528 



5 

* S 

PRINTED-CIRCUIT ASS'Y 

I00I54-I 



4 


CASE ASSY 

1001537 



3 


COVER ASSY 

1001534 



2 


PLATE-IDENTIFICATION 

' 1001543 . 






l-w 


LIST OF PARTS AN0 MATERIALS 


TEMPERATURE 
CONTROL- 
AMPLIFIER 
: ASSEMBLY / 


1000285 

IsHcrr I or I 


.} u • 

•1 • - 

'*■ ■ 
f # 












PROCUREMENT SPECIFICATION I PROCUREMENT SPECIFICATION 



ND*>1015404 General Specification, Configuration, 

Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
























6) 

6 






- i 


REPLACES PEI/ A W/tN 
CHANGES / UPGRADED 

class a tdrr C5&*o 


h^rLJ 


REVISED PER TDRR OS198 


W**M 


REVISED PER TDRR 11648 


m. 


REVISED PER TDRR 20731 










Section A A 


163 MAX 


4 


r 


.203 TYP 
REF 


-• 1.062 REF — 


B 


.5 MIN 

T~ 



r 


1 $ i i f 


122 

MAX 


.562 

REF 


e 


4 


j 


1.04-0 MAX. 


0 - +-.04 
■25 -.02 


REF 

~r~c~ 

1 T 


4-40NC-2A 

REF 


NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327, 

2. R2 TO BE SELECTED PEP ATP 1000285 AFTER 
IN/T/AL ENCAPSULATION. RANGE OF VALUES, FROM 

40.2. K THRU 121 < OF MS iN STEPS OF IKONMS. TWO RESISTORS MAY" 
BE USED TO GET /ALl/E HEEDED 
PER PART No. 1010694 

3 . IDENTIFY USING DRAW/NO No. } RE/iSION LETTER , SERIAL NO. AND 
' MANUFACTURERS SYMBOL. PER MIL -STD -ISO 

4. ENCAPSULATE Wirt/ EPOXY PER HD /002036 , CUR/NG CYCLE S 


to. 


J. ASSEMBLY TO MEET ALL REQUIREMENTS OF PS 1000285 


6. SOLDERING OF TERMINALS TO BE IN ACCORDANCE WITH MIL-STD-440. ALL OTHER 

ELECTRICAL CONNECTIONS, SOLDER PER MIL-S 6672 WITH SN60 WRAP2 50LDER PER 
QQ-S-571. . 

7. WltfDlfJG RESISTANCE FOR ACCEPTANCE TEST ING 

CONTROL WIHO/NO 1J5 ONMS S 25 ONMS 
TERMINAL 3 4 4- 

8. FINISHIVINYL WASH PER MIL-C-15328 AND 2INC CHROMATE PRIMER PER MIL-P-8585A, 
PAINT BLACK SEMI-GLOSS ENAMEL TT-E-529 CLASS B COLOR 27038 PER FED-STD-595. 


VIEW B-B VIEWC-C 

19. FOP TNE /0002185 - COO ASSEMBLY THE TYPE I PEQU/PEMEHTS OF THE PS AMO ATP 
SHALL APPLY IN MOTES 2 t 5, % lO, //, IE, 13,14 AMD IS OF THIS DPA\M/M$. 

20. FOP THE 1000Z8S-O/I ASSEMBLY THE TYPE IT AEQU IREMEATS OF THE PS AND ATP 
SHALL APPLY IN MOTES 2,5,9JO, H t /2,13,14 AND/5 OF THIS DMA WING. 

16. INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A .007 GRAY FIBER SHEET PER 
MIL-I-695A TYPE F WITH A MINIMUM DIELECTRIC STRENGTH OF 250 VOLTS PER MIL. 

17 SOLDER COVER ASSEMBLY TO CASE PER MIL-S-6872A WITH SN50 WRAP2 
SOLDER PER QQ-S-571. 

% R7 TO BE SELECTED PER ATP I0002BS PRIOR TO eNcaFSUlRTIOiZ. 

range OF VALUES, FROM 15 K THRU 24.9 H ONMS iH STEPS OF 100 oNmS 
TWO RESISTORS MAY 8E USED TO GET VALUE HEEDED . PER PART Ho. 10/0694 
RQ> TO BE SELECTED PER ATP 1000885 AFTER IM/T/AL eNcaPSi/l AT/0a/ 

RANGE OF VALUES, FROM 15* THRU 24.9K0NMS IN STEPS OF IOO ONMS 
TWO RESISTORS MAY SE USED TO GET /ALl/E NEEDED. PER PART No. 10/0694 
R!0 TO BE SELECTED PER ATP 100028 5 AFTER iN/T/AL ENCARSUlAT/O/Y 
range OF VALUES, FROM ION TNrU 24. 9* ONMS iN STEPS OF 100 ONMS 
TWO RESISTORS MAY SE l/SED TO GET VALUE NEEDED. PER FART No. 1010694 
RIB TO BE SELECTED FER ATP 1000285 AFTER /M/T/AL ENCAPSULATION 
RANGE OF VALUES } FROM 2K TNRU 8K ONMS iN STEFS OF 100 ONMS 
TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 10/0694 

13. R/4 TO BE SELECTED FER ATP 1000285 PR/OR TO ENCAFsUlAT/oN 
RANGE OF VALUES , FROM IONm TNrU 10 ONMS iN STEPS OF I OHM 

TWO RES/5 TORS MAY BE USED TO GET VALUE NEEDED. FER °ART //o. 10/0604- 

14. R3 TO BE SELECTED PER ATP 1000285 PRIOR TO ENCAPSULATION RANGE OF 
VALUES, FROM 300K THRU I MEGOHM TWO RESISTORS MAY BE USED TO GET 
VALUE NEEDED PER TART NO. I0IC693. 

15. Cl TO BE SELECTED PER ATP 1000285 PRIOR TO ENCAPSULATION RANGE OF 
VALUES FROM 30 THRU I40UF PER PART NO 1006789. 

18. CENTER IDENTIFICATION PLATE OVER 
POTTING HOLE. 


//. 


12 . 


r>? 

— ! SEE NOTE 20 





Jr 


SEE NOTE 19 





%/R 

WIRE 

GRAY FIBER SHEET 

1006711-13 

AWG30 

NOTE 16 

19 

18 

AR 

A/R 




x 

schematic 

100/533 


REF 


>< 

x 

WIRING ASSEMBLY 

100/53 5 


REF 


/ 

1 

RESISTOR 

1010693 

SAT 

NOTE 14 

17 

/ 

1 

RESISTOR 

1010604 

SAT 

NOTE *13 

16 

/ 

/ 

RES 1ST OR 

10/0694 

5/A T 

NOTE 12 

t5 

/ 

/ 

RESISTOR 

10/0694 

SAT 

MOTE // 

14 

/ 

/ 

RESISTOR 

10/0694 

SAT 

mote 9 

19 

/ 

! 

CAPACITOR 

1006709 

SAT 

NOTE 15 

1C 

5 

5 

DIODE 

1010 4 9 7 

500PIV 

3.4 W 

II 

/ 

i 

RESISTOR 

1010694 

5 A T 

NOTE 10 

10 

/ 

1 

RESISTOR 

1010694 

SAT 

NOTE 2 

9 

/ 

l 

TRANSFORMER 

1001532 



8 

/ 

1 

REACTOR ! 

1001531 



7 

/ 

1 

REACTOR 

1001530 



6 

/ 

1 

REACTOR ASSY 

1001528 



5 

/ 

i 

PRINTED - C/PCU/T A 5 5 »Y 

100154-1 



4 

/ 

l 

CASE ASSY 

1001537 



3 

/ 

i 

COVER ASSY 

1001534 



_2 J 

/ 

i 

PLATE-IDENTIFICATION 

1001543 



! 

-Oil 

-000 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

. J 


8 


1007056 


1010039 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 
TRACTIONS 


DO NOT SCALE THIS DRAWING 


LIST OF PARTS AND MATERIALS 


M I T 

INSTRUMENTATION LAS 
CONTRACT 


mm 




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TatT . 

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41A 

MNVIl 


M^JlL APPROVAL | 0ATE 


MSC 

lot- 


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TEMPERATURE 
CONTROL- 
AMPLIFIER 
ASSEMBL Y 


SCALE 

2/1 


-HTT- 

INSTRUMENTATION 

LABORATORY 


1000285 


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This specification consists of pages i 
to iv and 1 to IS inclusive. 



ND-1015404 General Specification, Configuration, 

Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment 

















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APOLLO GAN Specification 
PS-1000285-B . 

•UBSept. 1963 . A 4 


l 




TEMPERATURE CCBfTROL AMPLIFIER 

k /'A *;* i^ v .1 ^ 

V j: -v.V ‘ “’■.., ' •• * . '. ' V ,.".." .... 

y The purpose of this document is to establish the manufacturing and 
test requirements for procurement of Temperature Control Amplifiers 
for use in the Apollo Guidance and Navigation Equipment* 


4 ,.. 


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/». ■% ^jc 1 .* ^ 1 { 1 A , ♦ ■ 

> i . 4 ^ ■ fob ? ■** * ’' * 4 

temperature contrcmu amplifier 


•••y-v.v-” ■ •■. "r^”'j .fy.v. 


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A 

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1 ‘ • 4*a • 


PERATURE CONTRCNU AMPLIFIER a |- a ^ ' 

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A : ‘f A *' ,} ' K - A ; • 4’ » 1 


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L scope \. r ; ♦s -a * :.<'** ' ; v .« a?a 

* *’A *-♦ * ^ — ‘ - - AH% ; ’ V| 

1-1 PURPOSE. This specification establishes the requirements for the <a * a 
procurement of the Temperature Control Amplifier hereafter called A 1A 

amplifier. M ; . ., • " yfi •, 

‘ V , ^ ' t - ' V ' . ' " - *j 

i. APPLICABLE DOCUMENTS -a* : a i, * ..H*A; frk'« *a 1| j‘: a - 

■“ • a tv'A *%. ; vir 1 v ri w ' 1 y !j 4 ■ jr « 

3-1 EFFECTIVE SSSUE 8 . The folloeiag documente ef the ieene in effect Ay 
on the date of invitation# for bide form a pa.vt ef this specification tothe 
extent specified hsreia» ; , - . .v . %\r'- ’* 

spscmcATioNs " .' ''4 ; '. VA ^'.A' yV?" A^y j' 1 

•y , : <, - , A-- ^ ¥< ; V ''4'’ V w f . 


/ -• T,v. 

,v:4.-. ';y 4 4 ' t4, t '4 4 h 4 V << • , - 

Preservation,, Methods of t^-4 '*a?- ^ yy, 

v ; y ■ »* * *> v*> ’ } 

Electronic and Electrical Equipment j| 4 
; 1 4 ^ • and Associated Repair Parte, 4 ‘ijj- 

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APOLLO OAK Specification 
F*-1000*8*-* 

CIim k R«l«aa« 

TDRR 01266 

IS May 1063 r , 


APOLLO GAN Specification 
PS-100028S-B 
86 Sept. 1963 


APOLLO 0 A N Spocl/lcatieo 1 ?f 
PS-1000285-B , f 

M Sept. 1963 


PROCUREMENT SPECIFICATION 


PROCUREMENT SPECIFICATION 


TEMPERATURE CONTROL AMPLIFIER 


TEMPERATURE CONTROL AMPLIFIER 


TEMPERATURE CONTROL AMPLIFIER 


Date * I Letter 


|.Revision I TDRR I ; Pages 


No. I Revised 


10 Dee* *63 


21 Jaiu f 64| D 05860 I Pages * and 10. 


11 Feb.*64 


9 June '64 


25 Aug.*64 a 




Page 6 


This specification consists ef pages i 
W it and i to 1§ inclusive. 


I MIT I NASA 


Rev.”B” replaces 

26 Sept.*62 ' B &333H Rev."A* with 

changes. 


<*i 5 7 


06252 Pages 9.11 and 12 \jj 

.«*. lt ;,?-’- 10 - 11 Wf 


The purpose of this document la to establish the manufacturing and 
test requirements for procurement of Temperature Control Amplifiers 
for use in the Apollo Guidance and Navigation Equipment. 




MASA/MSC 


lulu 


L scope : 

1-1 PURPOSE. This specification establishes the requirements for the 
procurement of the Temperature Control Amplifier hereafter called 
amplifier. 

S. APPLICABLE DOCUMENTS > , 

1-1 EFFECTIVE ISSUES. The following documents of the issue in effect 
on the date of invitations for bids form a part of this specification to the 
extent specified herein. - 

SPECIFICATIONS . 


Military 
> MIL-F-U6 


MIL-E-175S6 


Apollo G 4 If 
ND-1002023 


ND-1002059 


ND-1015404 


Preservation. Methods of 

Electronic end Electrical Equipment 
and Associated Repair Parte. 
Preparation fer Delivery of 


Procedure for Serialisation of Components. 
Assemblies, eta., for Apollo GefcMSioe 
and Navigation equipment ... ! 

Qualification Specification, Magnetic : \ 
Amplifiers 

General Specification, Configuration, 
Process and Quality Control Requirements 
for Suppliers ef High Reliability Articles 
for Use in Spacecraft and Supporting i 
Equipment ■ - . * 1 ^ 


ND-1002019 


Markings General Specification for 


ii 


1 






This specification consists of pages i 
\o iv and 1 to 1ft inclusive. 







APOLLO GAN Specification 
PS-1000285- C 
8 6 Sept f 1 088" 

10 Dec. 1063 

3-2.4. 3 Marking. Marking shall be in accordance with MIL-STD-130 
am) Specification ND-1002018* amt m specified an the applicable drawing. 

, - . | *-♦ ->• -•**** ' -.f —’ ' ’ t y 1 t . %.<r# ; > ,. * V >«#> * - • 


3-2. 5 Serial Ifumbera Each amplifier identified by General Arrangement 
(or Assembly) Drawing shall be identified by a serial number assigned 
in accordance with Specification ND-1002023. 

3-2.6 Workmanship. The fabrication and finish of the amplifier, its 
assemblies, subassemblies, and parts shall be such as to produce a unit 
free from any defect that would affect proper functioning in service. 

3-2. 7 Warranty . A warranty shall provide for the supplier to remedy by 
correction or replacement any component or end item found to be defective 
in material or workmanship not later than six (•) months after acceptance. 
The allowability of the cost of any such correction or replacement shall 
be determined as provided in the clauses of the appropriate contract entitled 
"Allowable Cost, Fixed Fee and Payment, " and "Inspection and Correction 
of Defects." 

3-2.8 Service Life. 

3-2.8.1 Operating Life. The amplifier design is intended to meet perform¬ 
ance specifications for at least 20,000 hours of operation, excluding the 
supplier’s test time of the complete unit. 

3-2. 8.2 Shelf Life. The amplifier design is intended to have a shelf life 
of at least 5 years, without operation, at ambient room temperature 
after final acceptance at the supplier's plant, 

3-3 PERFORMANCE AND PRODUCT CHARACTERISTICS. The following 
requirements are stated to inform the supplier of specific characteristics 
and of the goals that were considered in the design. Inclusion of this 
information shall not be construed by the supplier as authorization to 
modify the design. 

If the design of any part is not completely specified by the contractual 
documents, the supplier may submit a suggested design document for 
approval which will support these requirements. 

If, in the opinion of the supplier, any design or testing shall impose 
undue time delay or expense, he shall so state, in detail, in a counter¬ 
proposal, substantiating all contributing factors when submitting a bid, 
proposal, or change request in connection with this specification. 

Requests for changes to or deviations from this specification or 
applicable drawings, specifications, publications, materials, or processes 
specified herein shall be accompanied by written justification. 


4 


APOLLO GAM Specification 
PS-1000285- 

Claes A Release 
TDRR 01266 
15 May 1963 


PROCUREMENT SPECIFICATION 
FOR 

TEMPERATURE CONTROL AMPLIFIER 


Date 

Revision 

Letter 

TDRR 

No. 

Pages 

Revised 


oval 

MIT 

NASA 

26 Sept.'6: 

B 

033 3 H 

r?plzcs£ 

Rev. "A" with ^ 
c h ci r*s ® s . 

M 

m 

?0 Dec.’63 

0 

05157 

Pege. 1% 2, 

thru 14; 15 added 

w( 

m 

21 Jan.*64 

D 

05860 

Pages 9 and 10. 

k)i 


11 Feb.*64 

8 ' 

06252 

Pages 9,11 and 12 

wit 

% 

9 June *64 

P 

omi 

Pages 5.9,10,11 
and 13* 

w. 

25 Aug.'64 

G 

IlMf 

Page 6 

w 

M 

15 Sept '64 

H 

12537 


m 

WJR 


This specification consists of pages I 
\o iv and 1 to 15 inclusive. 




APOLLO G 4 N Specification 

PS-1000285-B 

36 Sept. 1963 


TEMPERATURE CONTROL AMPLIFIER 


The purpose of this document is to establish the manufacturing and 
test requirements for procurement of Temperature Control Amplifiers 
for use in the Apollo Guidance and Navigation Equipment. 



'fkb/U 

MIT/IL 6 

DATE 


7/u/n 

NASA/MSC 

DATE 


ii 



APOLLO GAN Specification 
PS-1000285-B 
V Sept. 1963 


PREPARED BY 


TITLE 


DATE 



APOLLO GAN Specification 

PS-1000285-C 

t eSapi t i o e a 

10 Dec. 1963 


PROCUREMENT SPECIFICATION 
FOR 

TEMPERATURE CONTROL AMPLIFIER 



TABLE OF CONTENTS 


SECTIQIf 

TITLE 

PAGE 

1 

Scope 

i 

2 

Applicable Documents 

1 

2 

Requirements 

2 

4 

Quality Assurance 
Provisions 

8 

2 

Preparation tor Delivery 

* 14 

6 

Notes 

14 


iv 




APOLLO GAN Specification 
PS-1000285-B 

18 Sept. 1963 


PROCUREMENT SPECIFICATION 
FOR 

TEMPERATURE CONTROL AMPLIFIER 


U SCOPE 

1-1 PURPOSE. Thie specification establishes the requirements for the 
procurement of the Temperature Control Amplifier hereafter called 
amplifier. 

S. APPLICABLE DOCUMENTS 


3-1 EFFECTIVE ISSUES. The following documents of the issue in effect 
on the date of invitations for bids form a part of this specification to the 
extent specified herein. 

SPECIFICATIONS 


Military 
MIL-P-118 
MIL-E-17555 

Apollo GAN 
ND-1002023 

ND-1002059 

ND-1015404 


Preservation. Methods of 

Electronic and Electrical Equipment 
and Associated Repair Parts. 
Preparation for Delivery of 


Procedure for Serialisation of Components, 
Assemblies, etc., for Apollo Guidance 
and Navigation equipment 

Qualification Specification, Magnetic 
Amplifiers 

General Specification, Configuration, 
Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment 


ND-1002019 Marking, General Specification for 


1 



APOLLO GAN Specification 
PS-1000285 C 
10 Dec. 1963 


STANDARDS 

Federal 

FED-STD-595 
Military 

MIL-STD-130 

MIL-STD-20 2 

MIL-STD-810 

DRAWINGS 

Apollo GAN 
1000285 
1001529 

1001630 

1001531 

1001532 


Colora 


Identification Marking of U. S. 
Military Property 

Test Methods for Electronic and 
Electrical Component Parts 

Environmental Test Methods for 
Aerospace and Ground Equipment 


Temperature Control Amplifier 

Core A Coil Assembly (Reactor 1st Stage, 
Matched Pair) 

Core A Coil Assembly (Reactor 3rd Stage) 
Core A Coil Assembly (Reactor 2nd Stage) 
Core A Coil Assembly (Tra informer. Power) 


(Copies a f specifications, standards, drawings, and publications required by 
suppliers in connection with specific procurement functions should be obtained 
from the purchaser or as directed by the contracting officer.) 

2- 2 CONFLICTING REQUIREMENTS. In the event of conflict between the 
requirements of this specification and other specifications and drawings cited 
herein, resolution must be obtained from the MIT Apollo Management Office 
via the purchaser. 

3. REQUIREMENTS. 

The requirements of this specification are classfied under two headings: 

General Requirements which are defined in paragraph 3-2 and 
Performance and Product Characteristics whicn are defined in 
paragraph 3-3. 

3- 1 DESCRIPTION. The unit shall be a magnetic amplifier designed to 
provide accurate proportional control of the power to the IMU heatera, for 
precise and stable temperature control of the IMU. It shall provide stable 
operation when used in conjunction with the temperature control system and 
in closed loop operation with the controlled member. The output shall be 
used to drive s 2N1724 silicon power transistor in the switching mode of 
operation, utilizing pulse width modulation to minimize power dissipation 
in the transistor. 


2 



APOLLO G It N Specification 

PS-100G285-C 

SfrScpfr i. 

10 Dec. 1963 


3-2 GENERAL REQUIREMENTS. 

5*2.1 Qualification Teat . When specified by the purchaser, a represent** 
a t* ve sample of the amplifiers shall be manufactured using the methods 
and procedures proposed for the production lot. These shall be submitted 
to the NASA Inspector for qualification test at an activity designated in the 
contract or by the purchaser. 

These qualification tests are conducted to determine whether or not 
the amplifiers are being produced in compliance with the requirements 
of the contract, specification, and drawings. Failure of the amplifiers to 
meet these requirements may result in disqualification of the supplier as 
determined by NASA or the purchaser. 

Further production of the item by the supplier prior to approval of 
the purchaser or the completion of the qualification tests shall be at the 
supplier's risk. Requalification will be required at the discretion of NASA 
or the purchaser in the event that: (a) the supplier has modified the item. 

(b) the supplier has instituted a change in the material used or in his pro¬ 
cessing. or (e) the specification requirements for the item have been 
amended or revised sufficiently to affect the character of the item. 

The qualification tests will be conducted in accordance with the 
procedures specified in section 4 of this specification. 

5-2. 2 Requalification Test. When specified by the purchaser, the supplier 
shall submit one or more amplifiers to be selected from each production 
lot by the purchaser for submission to a designated testing activity to 
determine compliance of the sample (s) with the requirements of the contract, 
specification, and drawings. 

5-2. 3 Materials and Construction . The materials used in fabricating the 
amplifiers ahall be in strict accordance with the applicable drawings and 
specifications referenced herein. Substitute materials shall be selected 
of such quality as to ensure that the equipment will meet the requirements 
of this specification and shall be subject to prior approval of the purchaser. 

5*2.4 Weight, Dimensions. Finish, and Marking. The weight, dimensions, 
finish, and marking of the amplifier shall comply with the requirements 
specified herein or on the applicable drawings. 

5*2.4.1 Weight. Weight of the amplifier shall not exceed 3. 2 ounces. 

5"*- 2 Finish. Finish shall be as specified en the applicable drawing. 


3 



APOLLO G 4 N Specification 
PS-1000285-C 
38 Sept . 1008 
10 Dec. 1963 

3-2. 4. 3 Marking . Marking shall be in accordance with MIL-STD-130 
and Specification ND-1002018. and as specified an the applicable drawing. 


3-2. 5 Serial Numbers Each amplifier identified by General Arrangement 
(or Assembly) Drawing shall be identified by a serial number assigned 
in accordance with Specification ND-1002023. 

3-2. 8 Workmanship. The fabrication and fin sh of the amplifier, its 
assemblies, subassemblies, and parts shall oe such as to produce a unit 
free from any defect that would affect proper functioning in service. 

3“2. 7 Warranty . A warranty shall provide 'or the supplier to remedy by 
correction or replacement any component or end item found to be defective 
in material or workmanship not later than six (•) months afte** acceptance. 
The allowability of the cost of any such correction or replacement shall 
be determined as provided in the clauses of the appropriate contract entitled 
"Allowable Cost, Fixed Fee and Payment, " and "Inspection and Correction 
of Defects. " 

3-2.8 Service Life. 

3-2. 8.1 Operating Life. The amplifier design is intended to meet perform¬ 
ance specifications for at least 20,000 hours of operation, excluding the 
supplier's test time of the complete unit. 

3-2. 8 . 2 Shelf Life. The amplifier design is intended to have a shelf life 
of at least 5 years, without operation, at ambient room temperature 
after final acceptance at the supplier's plant. 

3-3 PERFORMANCE AND PRODUCT CHARACTERISTICS. The following 
requirements are stated to inform the supplier of specific characteristics 
and of the goals that were considered in the design. Inclusion of this 
information shall not be construed by the supplier as authorization to 
modify the design. 

If the design of any part is not completely specified by the contractual 
documents, the supplier may submit a suggested design document for 
approval which will support these requirements. 

If, in the opinion of the supplier, any design or testing shall impose 
undue time delay or expense, he shall so state, in detail, in a counter¬ 
proposal, substantiating all contributing factors when submitting a hid, 
proposal, or change request in connection with this specification. 

Requests for changes to or deviations from this specification or 
applicable drawings, specifications, publications, materials, or processes 
specified herein shall be accompanied by written justification. 


4 



APOLLO GAN Specification 
PS-100C285-F 
46 Dec. lU g fr - 
9 June 1964 


3-3.1 Functional Requirement!. 


« • i | Winding Resistances. DC resistance of the windings shall be as 
specifiei TinApo l lo U 1 - T Drh.ing 1000285. 1001529. 1001530. 1001531. and 
1001532. 

3-312 Dielectric Strength. The amplifier shall exhibit no evidence of 
breakdowfTwHen'subjected To a 500V rms voltage. 

3-3.1. 3 Insulation Resistance. The insulation resistance of the amplifier 
shall be 10 megohms minimum. 

S-S. 1. 4 Performance. Performance of the amplifier when used 1 " conjunction 
with Apoll o 0 AN ~~Firt Number 1010273 (2N1724 transistor) diall be as follows. 

3-3 1. 4.1 Power Input. The amplifier shall operate with 75 ma t 

current from a 20 ±2 V rma, 3200 ±32 cps source having the waveform character!# 

tics specified in 4-2. 2. 

3-3 1 4. 2 Gain. The amplifier shall have a minimum steady state gain trf 
46 watts/M snip'over the control rangelfrom 5 percent to 90 percent) of the 
maximum power dissipated by a 15.5 ohm resistive load. 

3-3.1. 4. 3 Transient Response. When the input is adjusted for a stable < 5 
minimum) output power level equal to 5 percent of po^r 

when the input is then increased by a step input of 0.7^ p amperes, the po 
dissipated in the load shall be as specified below: 

From t « 0 to t » 0.5 sec, the load dissipation shall increase within Ihm limits 
defined by twe curves whose equations are as fellows (where P is 
dissipation in watte and V' is the time lapse m seconds after the step input 
is applied): 

a) P * 22 + 6.38 t 

b) P » 2.09 + 15.5 t 

After a 0. 5 seoond interval has elapsed, the load.dlsslpation shall be' • • 

16.0 ± €.0 watts. Thereafter, the load dissipation shall increase within the 
limits defined by two curves whose equations are as follows: 

a) 22 40.3ft 

b) P* 10 4 0.22 t , * . 

The load dissipation shall reach a maximum of at least 4L5 

to continuous saturation of the 2N1724 transistor) between 61 and 140 seconds after 
the step input is applied. 

Transient response shall be as specified after reaching ^ermal sUbility 
with an ambient temperature of 25 5 ±5 6 C and again after reaching tnern ai 
stability with an ambient temperature of 65° ±5°C. When the ambient terope a 
ture is returned to 25° ±5°C and after thermal stabilization occurs, the amplifier 
shall again operate as specified* 




5 



APOLLO GAN Specification 
PS-1000285-B 
t a ge i; 1 8 09 
• 15 Auyl^M 

Transient response shall be as specified (with an ambient temperature 
of 25° ±5°C) after being subjected (non*operating) to the following vibration: 

5 g's (0 to peak), 5 cps to 2,000 cps to 5 cps at 1 minute per octave logrithmic 
sweep once along each of the 3 orthogonal axes, 0.12 inch double amplitude 
maximum. 

Transient response shall be as specified (with an ambient temperature 
of 25° ±5°C) after being subjected (non-operating) to a 50-g shock test in 
accordance with MIL-STD-810, method 513, procedure V. 

3-3.1. 4. 4 Transistor Base Current. When the input current is adjusted for 
maximum power output, the current supplied to the base of the 2N1724 transis¬ 
tor shall be at least 100 ma dc. 

3-3.1. 4. 5 Low Temperature Output. When an input of 1.60 ma is flowing through 
the amplifier from terminal 3 to terminal 4, the power delivered to the load 
shall be at least 48 watts. 

3-3.1. 4. 6 Null Offset. The amplifier shall have an input of 0.00 ±0. 43 u amp 
for 3 watts of load power dissipation. 

3-3. 2 Environmental Retirements. The amplifier shall be capable of meeting 
the requirements of Specification ND-1002059. When a particular requirement 
in Specification ND-1002059 includes amplifier operation while being subjected 
to an environment, this shall be construed to mean that the 20 V rms, 32C0 cps 
input shall not exceed 75 ma under standard operating conditions as defined in 
6-1. L 

3-3. 3 Design Requirements. 

3 3.1 Interchangeability. Unless otherwise specified, the amplifier and its 
component parts shall be physically and functionally interchangeable without 
selection or fitting. 

3-3. 3. 2 Reliability . The amplifier shall be capable of operating a minimum 
of 20,000 consecutive hours without maintenance under any combination of 
conditions specified herein and shall have a maximum failure rate of 0.5 failures 
per 1,000, 000 hours. 

3-3. 3. 3 Radio Interference Suppression. The suppression of radio noise and 
interference shall be considered in the design of the amplifier. 

3-3. 3. 4 Fl ammable Materials. Materials which may be ignited or cause an 
explosion - sliall not be used for construction applications where sparking or 
arcing could cause ignition. Materials which may inadvertently support com¬ 
bustion shall not be used. Flammable impregnating, potting or embedding 
compounds, when enclosed in fire-resistance containers, shall be acceptable. 

3-3. 3. 5 Toxic^ Materials. Materials which produce harmful toxic effects 
during service - usage shall not be used. Where a suitable nontoxic material 


6 



APOLLO GIN Specification 
PS-1000285-B 

26 Sept, 1863 


is not available, preventive measures shall be provided, subject to the 
approval of NASA. Materials which when ignited, produce toxic substances 
or vapors shall be avoided whenever practicable. 

3-3. 3. 6 Unstable Materials, Materials which are unstable or become 
unstable to the extent that they emit or deposit corrosive substances capable 
of causing corrosion or producing electrical leakage paths within an 
assembly under possible operating and storage conditions shall not be 
used during manufacture or recommended for use during maintenance. 

3-3. 3. 7 Corrosion, Moisture, and Fungus-Resistant Materials . Materials 
shall be selected for noncorrosive and nonhygroscopic characteristics 
and ability to resist the effects of corrosion, moisture and fungus. 
Preference shall be given to materials with inherent fungus resistance 
rather than reliance upon the application of surface fungistatic or fungicidal 
treatments. 

3-3. 3. 8 Dissimilar Metals. The use of dissimilar metals shall be 
avoided whenever practicable. Magnesium shall not be used except with 
prior approval of the purchaser or when so called for on the applicable 
Apollo GIN drawings. 


t 



APOLLO GAN Specification 

PS-1000285-B 

28 Sept. 1963 


4. QUALITY ASSURANCE PROVISIONS 

4-1 GENERAL. Unless otherwise specified herein, the supplier is 
responsible for the performance oi all inspection requirements prior 
to submission for NASA inspection and acceptance. Except as otherwise 
specified, the supplier may utilize his own facilities or any commercial 
laboratory acceptable to NASA. Inspection records of the examinations 
and tests shall be kept complete and available to NASA as specified in the 
contract or order. The supplier shall conform to Class 1 of Specifica¬ 
tion ND 1015404. 

4-L1 Acceptance Tests. These tests shall be accomplished on each 
amplifier being submitted for acceptance under the contract. Acceptance 
test data on each unit accepted must accompany shipment to the purchaser. 
Acceptance tests shall be witnessed by the cognisant government inspector, 
a representative of the purchaser, or as the purchaser may direct in the 
procurement order. These tests are detailed in paragraph 4-2. Failure 
of the amplifier to comply with these requirements shall result in rejection 
of the item or lot of items. 

4-L 2 Qualification and Requaliflcation Tests. Qualification and requali- 
fication tests shall be accomplished at a NASA designated activity. These 
tests, as outlined in paragraph 4-3, shall be conducted after the award of 
the contract to determine that the production will meet all requirements of 
this specification. Acceptance shall be based on no defects in the amplifier. 

Failure of the amplifier to comply with these requirements shall 
result in the rejection of the lot or the cessation of production, as 
determined by the procuring activity. 

4-2 ACCEPTANCE TESTS. 

4-2.1 Test Conditions. Unless otherwise specified herein, the amplifier 
■hall be subjected to tests under the following ambient conditions: 

Temperature 25 * 10<>C 

Relative Humidity Not more than 90% 

Barometric Pressure 28 to 31 in. Hg 

4-2. 2 Test Power. The following electrical inputs, as measured at the 
input of the unit under test, are necessary for testing this item: 

(a) 20 * 2V rms, 3200 * 32 cps, square wave, center tapped, 

1.0 va maximum power. The square wave shall have a 
rise time of 20 seconds maximum and a balanced duty 
cycle within 5.0 percent. 

(b) 18. 72 * 0. 20 vdc, 12 ma 

(c) 28.00 * 0. 28 vdc, 2 amp 


8 



11 Pebi 
• June Tfi&i 

4-2. 3 Visual and Mechanical Inspection. A comprehensive inspection shall 
be made of the amplifier to determine the extent of compliance with the re¬ 
quirement of this specification and the applicable Apollo GAN drawing speci¬ 
fied in Section 2 and shall at least include determination on the following: 

a) Size, Afcmension, tolerance, weight, appearance. and markings. 

b) Adequacy of materials, parts, and subassemblies; compliance with 
specific ratings, and conformance to applicable specifications. 

c) Finish, coatings, construction, markings, and nameplates, as applicable. 

d) Wiring, cabling, welding, soldering, color coding, and terminals, as 
applicable. 

e) Workmanship and cleanup. 

4-2. 4 Winding Resistances. DC resistance of the windings shall be tested 
using method 303 of MIL-STD-202 and shall be as specified on Apollo GAN 
Drawing 1000285, 1001520, 1001530, 1001531, and 1001532. 

4-2. 5 Dielectric Strength. Dielectric strength shall be checked by apply¬ 
ing a 500 V rms, 60 cps v c>Tt age between each terminal and the case and a 
200 V rms, GO cps (100 K source impedance) voltage between terminals 1 and 
3, between terminals 1 and 5, and between terminals 3 and 5. The leakage 
current shall not exceed 1.0 ma. This test shall be conducted in accordance 
with method 301 of MIL-STD-20 2. 

4-2. 8 Insulation Resistance. Insulation resistance shall be checked by apply¬ 
ing a 250 vdc voltage (current limited to 6 p amp) between each terminal and 
the case and between terminals 1 and 3, between terminals 1 and 5. and between 
terminals 3 and 5. The minimum acceptable resistance shall be 10 megohms. 
This test shall be conducted in accordance with method 302 of MIL-STD-202. 

4-2. t Performance. Performance of the amplifier shall be checked as 
follows* The test setup for these tests shall be as specified in Figure 1. 

Unless otherwise specified, switches SI, S2 and S3 shall be in the open 
position. 


4-2. 7.1 Power Input. The input current from the 20 V, 3200 cps source shall 
be monitored" at meter Ml during all of the Performance tests. It shall not 
exceed 75 ma under any conditions. 


APOLLO GAN Specification 
PS-1000285-? 

So p41 1082 

S I Jani 1 964 
9 June 1964 

20 *?V rms 



Rl, R2, R3 * 1^60 ohms each, 0.0W 

R4 s C-40 ohm decade resistance (Rubicon model 1015 or equlv.) 

R5 = 1540 ohms, 0.01< 

R6 a 0*44 ohm, li 
R7 s 2.°K, c t, iW 
R8 a 15.5 ohms, 3< # 75W 

Ml a 0-100 aa thermocouple milllammeter (Weston model 622 or equlv.) 

M2 a 0-30 vdc thermocouple voltmeter, 0.5* accuracy (or equivalent true ras meter) 

M3 = 0-150 ma clamp-on dc mllllammeter, 3^ accuracy 
M4 a Recording oscillograph (C.B.C. type 5-124 or equlv.j 150 cps 
- galvanometer frequency response) • 

M5 a DO ilcrc-voltneter (H.P. 4?5A with floated Input, or *qulv, ), See Note-2. 
Q1 a 2S1724 transistor meeting requirements of Apollo Dmwtng 1010273. 

KOTESi 1) Oscillograph (M4) shall be calIterated-to read the average 
voltage of a 6400 cp6 pulse width modulated 28 vdc waveform. 

2) This meter application Is highly critical and any equivalent 
meter shall be carefully evaluated. 


Figure 1. Test Setup 


10 



APOLLO G & N Specification 
PS-1000285-JT 
■iO P ee i 10 0 3 

V June 

4-2. 7. 2 Gain .. Adjust variable resistor R4 to a value which gives a load 
voltage (as indicated at meter M2) of 23 ^1V rms (24 watts). Readjust R4 to a 
value which gives a load voltage of 6.8 *0.3V rms (2 watts), as.indicated on M2. 
The two values of R4 obtained shall be within 0.44 ohm of each other and both 
values shall be between 17.0. and 23.. 0 ohms. NOTE! The output reading, at M2, 
should be taken after it becomes stable (2 minutes minimum),. 

4-2. 7. 3 Transient Response . Close switch S2 and adjust R4 for a stable 
(5 minutes minimum) voltage reading of 1.30 vdc as indicated cm the oscillo¬ 
graph (M4). Apply a step input by closing switch S3. The load voltage, as 
measured on M4, shall be as specified in Figure 2 and shall steadily increase 
until it reaches its maximum. M4 shall be calibrated in volts average. 


This test shall be performed five times; once after the amplifier reaches 
thermal stability under each of the following conditions, in the sequence indi¬ 
cated: 


a) An ambient temperature of 25° ±5°C. 

b) An ambient temperature of 65° ±5°C. 

c) An ambient temperature of 25° ±5°C. 

d) An ambient temperature of 25° *5°Q: and after being subjected 

(non-operating) to a vibration test as follows: 5 g's (0 to peak), 
5 cps to 2,000 cps to 5 cps at 1 minute per octave logarithmic 
sweep along each of the 3 orthogonal axes, 0.12 inch double 
amplitude amximum. 

e) An ambient temperature of 25° ±5°C; and after being aibjected 

(non-operating) to a shock test as follows: method 516 of 
MIL-STD-810, procedure V, except that a 50-g shock shall be 
used. 


11 



2.4V 


£ — £. V.' c J — 

10 B e* . 10 < 

11 Peb. 196 


t 




li- 


|Z7: 


*i;5t 



DEPINIHG BQUATIONS 


t=tlme In seconds after 

Time 

Touation 1 

step input applied 

•300 to 0 sec 


Pspower dlssloated In 
load (watts) 



0 to 0*5 see 

P max* 22 4 °* 56t 

* This ralue shall be 
set after determining 
the saturation ralue 


P mln= 2 * 05 ♦ 

0.5 seo to sat. 

P .ax* 22 4 °* 56t 

and shall be between 

2.05V and 2 . 62 V. 

** 41.5V minimum 

0.5 to 140 sec 


140 to 300 sec 



Figure 2. Transient Response 


12 

















APOLLO GIN Specification 
PS-1000285- r 
*9 S e p t, lo ss 
I S P e e. 1 9 00 
• June 1964 


4-2. T. 4 Transistor Base Current. 
(M2), The transistor base current. 

at least 100 ma dc. 


Adjust R4 for maximum load voltage 
as indicated at meter M3, shall be 


f:?- 7 '* V w> J e mper »ture Outmit. Adjurt R4 to 20 ohm* and move .witch 
SI to the closed position. The load voltage (M2) shall be at least 26V rma» 

® Null Offset. Adjust R4 for a null of the bridge output aa indicated 
by a minimum voltage soil50essthaniD ft volts). Note the value of R4. Readjust R4 for 
output of 6.8V rms as indicated on M2. Again note the value of R4. The 
two values of R4 shall not differ by more than 0.25 ohm. 

4-3 Qualification and Reo uallfication. Qualification and requalification 
tests shall be performed in accordance with Specification ND-1002059. 

When amplifier operation is included as a condition in a test in Speci¬ 
fication ND-1002059. the amplifier shall be operated under standard 
operating conditions (see 6-L1). The input (terminals 1 and 2) shall be 
monitored during operation under standard operating conditions and shall 
not exceed T9 ma at any time. 


4 “ 4 Rell * Mli *y» The reliability requirements contained in Section 3 of 
this specification are design objectives. Unless specifically called for 
in the procurement contract, it shall not be necessary for the supplier 
to deinonstrate his compliance with the requirement. The supplier will 
furnish the purchaser or NASA such data as he may have available for 
establishing the current reliability of thes units. Additional data shall 
be accumulated to as great a degree as possible from the tests specified 
herein or any other tests the supplier may conduct which will tend to 
support or verify attainment of the reliability objectives specified. 


19 



APOLLO GAN Specification 

PS-100028£-C 

I f Sop ti 10 8 » ■ 

10 Dec. 1933 


ft. PREPARATION FOR DELIVERY 

5-1 PRESERVATION AND PACKAGING. The amplifier ehall be preserved 
and packaged in accordance with Specification MIL-E-17555, level B, as 
specified in the contract or purchase order. 

5-L1 Level B (Limited Military Packaging). Level B packaging is that 
which will afford adequate protection against damage during multiple 
domestic shipment, handling, and covered storage. 

5-1.1.1 Cleaning. Cleaning for Level B preservation and packaging shall 
be in accordance with method C-l of Specification MIL-B-116. 

5-L 1.1 Unit Protection. The amplifier shall be individually afforded 
unit protection in accordance with method III of Specification MIL-P-116. 

In addition, equipment packaged for level B protection shall be sealed 
against water and dust means of suitable wrapping. 

5-2 REPAIR PARTS. Rppair parts shall have preservation and packaging 
per the applicable repaiB parts list and its packaging supplement. 

5-3 PACKING. The eauipment shall be packed in accordance with 
Specification MIL-E-17»ftft, level B« 

5-4 MARKING. In addition to any special marking required by the 
contract or order, the marking of unit, interior packages, and exterior 
shipping containers shall be in accordance with level B of Specification 
MIL-E-17555. 

6. NOTES 

8-1 DEFINITIONS. 

8-1.1 Standard Operating Conditions. For the purposes specified in 3 - 3 . 2 
and 4-3, standard operating conditions shall be defined as follows: The 
amplifier shall be connected to the test equipment and inputs as specified 
in Figure 1 with resistor R4 set at 5 ohms and switches SI, S2 and S3 in 
the open position. 


14 



APOLLO GAN Specification 
P*-1000285- C 

— ftapt t 1 969 

10 Dec. 1963 


Notice: When NASA drawings, specifications, or other data 

are used for any purpose other than in connection 
with a definitely related NASA procurement operation, 
• NASA thereby incurs no responsibility nor any 
obligation whatsoever; and the fact that NASA may 
have formulated, furnished, or in any way supplied 
the said drawings, specification, or other data 
is not to be regarded by implication or otherwise 
as in any manner licensing the holder or any other 
person or corporation, or conveying any rights or 
permission to manufacture, use, or sell any patented 
invention that may in any way be related thereto. 


IB 



V 


APOLLO G & N Specificatior 
PS-1000285-J 


Class A Release 
TDRR 01266 
15 May 1933 


PROCUREMENT SPECIFICATION 
FOR 

TEMPERATURE CONTROL AMPLIFIER 



Revision 

Letter 

Tnpn 


ADorc 

>val _ 

Date 

No. 

Revised 

MIT 

NASA _ 

in 

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£>33 3 H 

0 C 1 C T 

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Pages 9 n ud 10. 

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Pages 9,11 and 1' 


9 June 

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and 15. 


25 Aug.*6A 

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15 Sept *64 

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12537 


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8 July ’65 

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B 


This specification consists of pages i 
to iv and 1 to 15 inclusive. 




















APOLLO G&N Specification 
PS1000285-J 


PROCUREMENT SPECIFICATION 
FOR 

temperature control amplifier 


1. scope 

1 l PURPOSE. This specification establishes the requirements for the procurement 
of the Temperature Control Amplifier hereafter called amplifier. 

i 2 CLASSIFICATION. The requirements for the equipment covered by this specification 
shall ^ rsifledTfollmvs. Unless identified by the respective type, all requirements of 
this specification are applicable to all types. 

a Tvpel: The requirements for Part Numbers 1000285-000 shall be designated as 
Type i in this specification and identified as PS100028»-000. 
b. Type II: The requirements for Part Number 1000285-011 shall be designated a. 
Type H in this specification and identified as PS1000285-011. 

2. APPLICABLE DOCUMENTS 

2 1 EFFECTIVE ISSUES. The following documents of the issue m effect 
of invitatiwus for bids form a par, of this specification to the extent specified herein. 


SPECIFICATIONS 


Military 

MIL-P-H6 

MIL-E-17555 


Preservation, Methods of 

Electronic and Electrical Equipment and Associated 
Repair Parts, Preparation for Delivery of 


APOLLO G&N 
ND-1002023 

ND-1002059 
ND-1015404 


ND-1002019 


Procedure for Serialization of Components, Assemblies, 
etc., for APOLLO Guidance and Navigation Equipment 

Qualification Specification, Magnetic Amplifiers 

General Specification, Configuration, Process and 
Quality Control Requirements for Suppliers of High 
Reliability Articles for Use in Spacecraft and 
Supporting Equipment 
Marking, General Specification for 


1 




APOLLO G & N Specification 
PS - 100C285-J 


3-3.1 Functio nal Requirements. 

wrwrts* - 

1001532. 

3.3 I 2 Dielectric Strength. The amplifier snail exhibit no evidence of 
r.reakdo'.vrrwHen'suDjeccedTb a 500V rms voltage. 

t-3.1. 3 Insolation Res istance . The insulation resistance of the amplifier 
shall be 10 "megohms minimum. 

source (type H having the waveform characteristics specified in 4 2.2. 

3-3 14 2 Gain. The amplifier shall have a minimum steady state/gain of 
46 watts /m amp”over the control rangeUrom 5 percen* to 90 percent) of the 
maximum power dissipated by a 15.5 ohm resistive load. 

3 3 14 3 Transient Response. When the input is adjusted for a stable (E minutes 

ttiis S3-?S5FH.-5Tx. r .«»-“•-ssirs vss 

when the input is then increased by a step input of 0.7o p amp , t 
dissipated in the load shall be as specified below: 

From t * 0 to t * 0.5 sec, the load dissipation shall increase with:\ l ^Id * ” 

defined by two curves whose equations are as follows (where 
dissipation in watts and V is the time lapse in seconds after the step inp 
is applied): 

a) P * 22 + 0.36 t 

b) P * 2.05 + 15.9 t 

After a 0. b second interval has elapsed, t*e lo^.f 1 •dissipation anall be . • 

1G.0 -r f .0 watts. Thereafter, the load dissipation shall increase within , 
limits defined by two curves whose equations are as follows: 

a) F * 22 + 0.361 

b) P * 10 4- 0.22 t , . . . 

The load dissipation shall reach a maximum of at least 41 5 

to continuous saturation of the 2N1724 transistor) between 6 . and 140 seconds aft 
the step input is applied. 

Transient response shall be as specified after reaching thermal stability 
with an ambient temperature of 25 ±5 C and again a ^" n r ®® E C ^"| i p* l ‘'"e mpera - 

ture 1 is "returned toZ^l^cVnTJter thermal stabilization occurs, the amplifier 
shall again operate as specified. 


5 





APOLLO G & N Specification 
PS-1000235-# 


Transient response shall be as specified (with an ambient temperature 
of 25° ± 5 °C) after being subjected (non-operating) to the following yibratio . 

5 . 1 , (0 to peak), 5cps to 2,000 cps to 5 cps at 1 minute per octave logrithmic 
sweep once along each of the 3 orthogonal axes, 0.12 inch doable amplitude 
maximum. 

Transient response shall be as specified (with an aml ient temperature 
of 25° ±5° C) after being subjected (non-ope.-atirg) to a oO-g shock test m 
accordance with MIL-STD-810. method 513, procedure V. 

3-3 14 4 Transistor Base Current. When the input current is adjusted for 
maximum P bive?ourput7 fh^-cuF7-ent supplied to the base of the 2Ni724 transts- 
tor shall be at least 100 ma dc. 

3-3 1 4. 5 Low Temperature Output. When an input of 1.00 ma is flowing through 
the amplifieFTrorn Terminal Tto lerrr.inal 4. the power delivered to the load 
shall be at least 48 watts. 

3-3.1. 4. 6 Null Offset. The amplifier shall have an input of 0.00 ±0. 42 ji nmp 
for 3 watts of loacTpbwer dissipation. 

3-3 2 Environmental Requirements. The amplifier shall be capable of meeting 
the require me nTs'cTBpecifi cat I on~NI> -100 2059. When a particular requirement 
in Specification ND-1002059 includes amplifier operation while being subjected 
to an environment, this shall be construed to mean that the 20 V rms (Type I), or 
21V rmi (Type II), 3200 cps Input shall not exceed 75 ma under standard operating conditions 
as defined in 6-1.1. 

3-3. 3 Des ign Requirement s. 

3 3 1 Interchangeability. Unless otherwise specified, the amplifier and its^ 
compo nent part/ sKsOrte physically and functionally interchangeable without, 
selection or fitting. 

3-3 3 2 Reliability. The amplifier shall be capable of operating a minimum 
of 20,000 conl^Uitve hours without maintenance under any combination of 
conditions specified herein and shall have a maximum failure rate of 0.5 failures 
per 1 , 000 , 000 hours. 


3-3. 3. 3 Radio Inte rference Suppression. 
interference shairBe considered in the d€ 


The suppression of radio noise and 
ign of the ampliiier. 


3-3 3.4 Flammable Materials. Materials which may be ignited or cause an 
explosion shall not be used for - construction applications where sparking or 
arcing could cause ignition. Materials which may inadvertently su PP°rt com¬ 
bustion shall not be used. Flammable impregnating, potting or ^ 

compounds, when enclosed in fire-resistance containers, shall -.e acceptable. 

3-3 3 5 Toxic Materials. Materials which produce harmful toxic effects 

during sefVicif visage - shall not be used. Where a suitable nontoxic material 


6 










APOLLO G & N Specification 
PS-1000285-J 


4. QUALITY ASSURANCE PROVISIONS 

4-1 GENERAL. Unless otherwise specified herein, the supplier is 
responsible for the performance of all inspection requirements prior 
to submission for NASA inspection and acceptance. Except as otherwise 
specified, the supplier may utilize his own facilities or any commercial 
laboratory acceptable to NASA. Inspection records of the examinations 
and tests shall be kept complete and available to NASA as specified in the 
contract or order. The supplier shall conform to Class 1 of Specifica¬ 
tion ND 1015404. 

4-1 1 Acceptance Tests. These tests shall be accomplished on each 
amplifier being submitted for acceptance under the contract. Acceptance 
test data on each unit accepted must accompany shipment to the purchaser. 
Acceptance tests shall be witnessed by the cognizant government inspector, 
a representative of the purchaser, or as the purchaser rnay direct m the 
procurement order. These tests are detailed in paragraph 4-2. Failure 
of the amplifier to comply with these requirements shall result in rejection 
of the item or lot of items. 

4-1. 2 Quali fication and Requalification Tests. Qualification and requali- 
ficationtests shall be accomplished at a &ASA designated activity. These 
tests, as outlined in paragraph 4-3, shall be conducted after the award of 
the contract to determine that the production will meet all requirements of 
this specification. Acceptance snail be based on no defects in the amplifier. 

Failure of the amplifier to comply with these requirements shall 
result in the rejection i the lot or the cessation of production, as 
determined by the procuring activity. 

4-2 ACCEPTANCE TESTS. 

4-2.1 Test Conditions. Unless otherwise specified herein, the amplifier 
shall be subjected to tests under the following ambient conditions: 

Temperature 25 * 10°C 

Relative Humidity Not more than 90% 

Barometric Pressure 28 to 31 in. Hg 

4-2. 2 Test Power. The following electrical inputs, as measured at the 
input of the unit under test, are necessary for testing this item: 

(a) 20 ± 2V rms, .(Type II or 20+4, -2V rms (Type II) 3200 ± 32 cps, 
square wave, center tapped, 1.0 va maximum power. The square wave 
shall have a rise time of 20 p seconds maximum and a balanced duty 
cycle within 5.0 percent. 

(b) 18. 72 * 0. 20 vdc, 12 ma 

(c) 28. 00 * 0. 28 vdc, 2 amp 


8 








APOT.LO j $ N T necl ficatl 

-j 


4-2 3 Visual and Mechanical Inspection. A comprehensive inspectipn shall 
be made of the amplifier to determine the extent of compliance *ith the re 
quirement of this specification and the applicable Apollo G IN drawing speci¬ 
fied in Section 2 and shall at least include determination on the following: 

a) Size, dimension, tolerance, weight, appearance, and markings. 

b) Adequacy of materials, parts, and subassemblies: compliance with 
specific ratings, and conformance to applicable specification . 

c) Finish, coatings, construction, markings, and nameplates, as applicable. 

d) Wiring, cabling, welding, soldering, color coding, and terminals, as 
applicable. 

e) Workmanship and cleanup. 

4-2 4 Winding Resistances. DC resistance of the windings be tested 

using meth od 30 1 1 of M l l^ST D-202 and shall be as specified on Apollo G fc N 
Drawing 1000285, 1001529, 1001530, 1001531, and 1001o32. 

4-2 5 Dielectric Stremth. Dielectric strength shall be checked by applv- 
ing a S OO V rms ^BO cps vbTtage between each terminal and the case and a 
200 V rms, 30 cps (100 K source impedance) voUagebetweenteririmas an 
3 between terminals 1 and 5, and between terminals 3 and 5 The leakage 
current shall not exceed 1.0 ma. This test shall be conducted in accordance 
with method 301 of MIL-STD-202. 

4-2 6 Insulation Resistance. Insulation resistance shall be che cked by apply - 
ini?’a 2 r 0 vdc volt ageTcurrent limited to 5 ^ amp) between eacl \ t ® rmi ^ ® n< L 
£* case and between terminals 1 and 3, between terminals 1 and 5 and between 
terminals 3 and 5. The minimum acceptable .resistaMe shall ^ • 

This test shall be conducted in accordance with method 302 of MIL bTD 4U4. 

4-2 7 Performance. Performance of the amplifier shall be checked as 
follows- The tesFsetup for these tests shall be as specified in Figure 1. 

LnleL otherwise specified, switches SI, S2 and S3 shall be in the open 
position. 

4-271 Power Input. The inout current from the 20 V rms (Type I) or 21V rms (Type II) 
3200 cps source shall be monitored at meter Ml during all the Performance tests. It shall 
not exceed 75 ma under any conditions.- 


9 








APOLLO G&N Specification 
PS-1000285-J 

20±2V rms, Type I • 
or 20+4, -2V tits Type II 


















































Apollo GAN Specification 

PS-1000285 

15 May 1965 

Class 6 Release 

TDRR 



Apollo G A V Specification 
PS-1000285 
15 May 1963 


1 

$ 


t 


Apollo GAN Specification 

PS-1000285 

15 May 1963 


PROCUREMENT SPECIFICATION 
TEMPERATURE CONTROL AMPLIFIER (PA36A-1) 


PROCUREMENT SPECIFICATION 
FOR 

TEMPERATURE CONTROL AMPLIFIER (PA36A-1) 


Record of Revisions 


Revision 

Letter 

TDRR 

No* 

£ages 

Revised 

1 Approvals 

BATE 

KIT 

NASA 









f 2 





























Tlhis specification consists of Page 1 to iii and 
1 to 5 inclusive* 




TEMPERATURE CONTROL AMPLIFIER (PA36A-1) 


= i, 

\i 


The purpose of this document is to establish the manufacturing 
and test requirements for procurement. The Temperature Control 
Amplfier (PA36A-1) is Intended for use in the Apollo Guidance 
and Navigation Equipment program* 


i 



1. SCOPE 

1.1 This specification establishes the requirements for the procurement 

of the Temperature Control Amplifier (PA36A-1), hereinafter called the 
amplifier. 

2. APPLICABLE DOCUMENTS 

2.1 The following documents of the issue in effect on the date of invitation 
for bids form a part of this specification to the extent specified herein. 

SPECIFICATIONS 
Military 

MIL-T-27 
MIL-P-116 
MIL-I-16 910 

MIL-P-17555 


Transformers and Inductors 

Preservation, Methods of 

Interference Measurement, Radio, 
Methods and Limits, 14 Kilocycles to 
1000 Megacycles 

Electronic and Electrical Equipment 
and Associated Repair Parts, Prepara¬ 
tion for Delivery of 



iasa/mso approval 


Apollo G & N 


General Specification, Configuration, 


ND-1015404 General Specification, Configuration, 

Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment 


1 


ii 


1 







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irwsaBM, 



4 EQ. SPACES AT ^ 

UQtJ-CUMULATIVE -- 




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K&/& u,n/ 

P£R TT>KK 0%£C<> 

trOcTLZ, 


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MAX . 

~\ hr - * 375 * 



.5*2 t.09 MAX 


4 -- 4 -ONC- 2 A 
CRES MT& stud 
2 RECC'D 


REVISIONS 

DESCRIPTION 


. input s 


0—>«»' 20 / ttoy. rms :~;::~ 

>3200 - : _i 

(D->u>J 5 <?- 

® ■ > 

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® * l z.0^/O / TELEMETRY' 

_ OUTPUT—— — 

<D—»J 


FEED RACK 
RESISTOR 


.FOR DETAILED SPECIFICATIONS $£E 
PROCUREMENT' SPECIFICATION 1000236 



FOR INFORMATION ONLY 

CUSS B RELEASE TOR No .&&££— DATE 0 r 

| I | UNLESS OTHERWISE SPECIFIED 


NOMENCLATURE 
OR DESCRIPTION 


PART OR •MMMCATtfMi 

I IDENTIFYING NO. 

LIST OF PARTS AND MATERIALS 


MATERIAL 
OR NOTES 


M I T 

INSTRUMENTATION LAN 


DIMENSIONS ARC IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

ANHOVCO 

CH'CKCO 

CONTRACT 

NAS 9153 

“TOT 

■"jV-Fj 

DO NOT SCALE THIS DRAWING 

■— MMWM 

Afl’HOVlO 

fo| MSC 


MATERIAL: 


TJjl 

'Jo 


1 MITYIL APPROVAL 

I DATE 


HEATER CURRENT 
I AMPLIFIER _ —I 


CODE IDENT. 


INSTRUM ENT ATION 
LABORATORY 

Cammiom. Ma—. 


SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

1000286 




APPLICATION 


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REPLACES REV A WITH 
CHANGES 8 UPGRADED 
CLASS A.TDRR OSfCi. 




©0 ° ©e) k© 

b~*Jr —^© 


VIEW WITH COVER 
REMOVE0 



SECTION A-A - 



1 INTERPRET DRAM** /t/ ACCORDAaJCE lY/r/M/L-D-70327 ' . . 

Z.R3i R+ TO BE SELECTED PER ATP /OOOS8G * FT ^!f C * CA/ * Sl ' L A ri0 " 

* 3<rM 7 «o*,s m/ S ™ *so»/»,s 

" PER PART RO. 10103/!. OA/LY OA/e RES/STVR MAY BE USED. . 

RES/STOR PURU/SA/ED BY VEf/DUR ^ _ _ 

4.IDENTIFY USING DRAWING NO., REVISION LETTER, SERIAL NO. ft MANUFACTURERS 
SYMBOL. PER MIL-STD-ISO. . 

5. ENCAPSULATE WITH EPOXY PER ND1002036, CURING CYCLE B. 

6. ASSEMBLY TO MEET REQUIREMENTS OF PS 1000286. 

7. USE SN60 SOLDER PER 0Q-S-57I FOR ALL ELECTRICAL CONNECTIONS. 

8. USE SN50 SOLDER PER QQ-S-571 TO SOLDER COVER TO ASSEMBLY TO CASE. 

9. FINISH: VINYL WASH ft 2INC CHROMATE PRIMER PER MIL-P-6889 TYPE I. . 


WIRING ASSEMBLY 

IOOI619 

REF 

SCHEMATIC 

IOOI&22 

REF 

RESISTOR 

SAT. 

SEE NOTE 

TRANSFORMER 

1001623 


REACTOR ASSEMBLY 

1001620 


rpiUreo circuit assemsy 

looiOie 


CASE ASSEMBLY 

1001647 


COVER ASSEMBLY 

1001616 


PLATE - IDENTIFICATION 

1001543 



_ 1000286 

NCXT AMV U«CD 0* 

«mJCAT»N 


LIST OF PARTS ANO MAT RIALS 

HEATER CURRENT 
AMPLIFIER 
ASSEMBLY 

CALE | UMT WT I OOOC IOERT. 


INSTRUMENTATION 

LABORATORY 


SPACECRAFT CENTER 
HOWTO* TtXAA 

1000286 




































































Apollo C A N Specif 
PS-10OT286 “ 

IS May 1963 


Apollo G f, N Specification 
PS-1000286-A 
IS May 1963 
Class B Release 
TDRR OIJ.UC- 


Apollo G ft 1 Specification 
PS-1000286 
15 May 1963 


PROCUREMENT SPECIFICATION 
HEATER CURRENT AMPLIFIER (MA20A-1) 


PROCUREMENT SPECIFICATION 
FOR 

HEATER CURRENT AMPLIFIER (MA20A-1) 


Record of Revisions 



This specification consists of Page i to ill and 
1 to S inclusive. 


fl£\l x RfPLAceP 6V Rev’s" 

UjfTU CrHAt/GE S 


SATURABLE REACTOR 
HEATER CURRENT AMPLIFIER (MA20A-1) 


The purpose of this document is to establish the manufacturing 
and test requirements for procurement. The Heater Current Am^ifier 


Equipment program. 




SCOPE 

This specification establishes the requirements for the procurement 
of the Heater Current Amplifier (MA2QA-1), hereinafter called the 
amplifer. 

APPLICABLE DOCUMENTS 

The following documents of the issue in effect on the date of 
invitation for bids focm a part of this specification to the extent 
specified herein. 

SPECIFICATIONS 

Military 

MIL-T-27 Transformers and Inductors 

MIL-P-116 Preservation, Methods of 

MIL-I-16910 Interference Measurement, Radio, Method: 

and Limits, 14 Kilocycles to 1000 
Megacycles 

MIL-P-17555 Electronic and Electrical Equipment and 

Associated Repair Parts, Preparation foi 
Delivery of 

Apollo G(N 

ND-1015404 General Specification, Configuration, Pi 

eesr and Quality Control Requirements f< 
Suppliers of High Reliability Articles i 
use in Spacecraft and Supporting Equips 

STANDARDS 

Military 

MIL-STD-810 Environmental Test Methods for Aero¬ 

space and Ground Equipment 

DRAWINGS 

NASA 

1010039 Apollo IMU Temperature Control System, 

Scyematic 

1000286 Heater Current Amplifier (MA20A-1) 


1 

















































t lUTERPRET DRAWING ///ACCORDANCE W/rN Af/L-D- 703B7 

l. R3 4 R+ TO BE SELECTED PER ATP IOOOE &6 AFTER iS/T/AL EjJcAPSl/LATIOJf 
RANGE OF VALL/ES x FROM ?0K rURU HO K OUMS /U STEPS OF 
_ TWO RESISTORS MAT BE USED T 9 GET VALUE SEEDED. PER PART ¥ 0 . /O/O 36 + 

%, R 8 (EXTERNAL FEEDBACK RES/STOP) TO BE SELECTED PER ATP /000E3G ™ , . , / / 

RANGE OF VALUES FROM 300 OUMS rURU EK 0 UmS /U STEPS OF BO QUMS aUd 3< TmRU 7K OEMS m STEPS OF SO OHMS 
. 7 .: PER PART Mi.1010311. ONLY OUE RESISTOR MAY BE USED. 

RESISTOR FURNlSSED BY VENDOR 

4. IDENTIFY USING ORAWING NO., REVISION LETTER, SERIAL NO. 8 MANUFACTURERS 
SYMBOL. PER MIL-STD-ISO. 

5. ENCAPSULATE WITH EPOXY PER ND1002036, CURING CYCLE B. 

6. ASSEMBLY TO MEET REQUIREMENTS OF PS 1000286. 

7. USE SN60 SOLDER PER 0Q-S-57I FOR ALL ELECTRICAL CONNECTIONS. 

8. USE SN50 SOLDER PER OQ-S-571 TO SOLDER COVER TO ASSEMBLY TO CASE. 

9. FINISH I VINYL WASH 8 AINC CHROMATE PRIMER PER MIL-P-6889 TYPE I. 


oDIto 



" 3 ^- 

T:! 




































ND-1015404 General Specification, Configuration, 

Process and (^jality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment. 






































notes: 

I. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL*D'70327 
L R3 S R4 TO BE SELECTED PER ATP 1000286 AFTER INITIAL ENCAPSULATION 

,1 Range of values, from 90k thru iiokohms 

I TWO RESISTORS MAY BE USED TO GET VALUE NEEDED* PER PART NO. 1010695 
4, R 8 (EXTERNAL FEEDBACK RESISTOR) TO BE SELECTED PER ATP 1000286 
RANGE OF VALUES FROM 500 OHMS THRU 2K OHMS PER PART NO. I0I03II 
I ONLY ONE RESISTOR SHALL BE SELECTED AND THE PART NO. ANO DASH NO. SHALL 
1 BE MARKED ON THE COVER, AS SHOWN, PER NO 1002019 5 NDI002I22 TYPE IE CLASS 1 
4. IDENTIFY USING DRAWING NO., REVISION LETTER, SERIAL NO. 4ND 
MANUFACTURERS SYMBOL. PER MIL-STD-130 
•* ENCAPSULATE WITH EPOXY PER NO 1002036, CURING CYCLE B 

6 . ASSEMBLY TO MEET REQUIREMENTS OF PS 1000286 

7. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE WITH MIL-STD‘440 
WITH SN60WARP2 SOLDER. PER QQ-S-571 

B. SOLDER COVER ASSEMBLY TO CASE PER MIL'S’6S72A WITH SN50WARP2 SOLDER 
PER QQ-S-571 

f. FINISH*. VINYL WASH PER MIL-C-15328 AND ZINC CHROMATE PRIMER PER MIL'P~8585A 
' PAINT BLACK SEMI GLOSS ENAMEL TT-E’529 CLASS B. 

COLOR 27038 PER FED STD 595 

10. R7 TO BE SELECTED PER ATP 1000286 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 500 OHMS THRU IOKOHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO 1010694 
9 . CENTER IDENTIFICATION PLATE OVER POTTING HOLE 
8 * WINDING RESISTANCE FOR ACCEPTANCE TESTING; 

TERMINALS; 3 5 4 0.05 OHM MAX 
* 5 5 6 0.05 OHM MAX 

13. INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A .007 GRAY FIBER SHEET 
PER MIL-I-695A TYPE F, WITH A MINIMUM DIELECTRIC STRENGTH OF 
250VOLTS PER MIL 














































€ 



REPLACES RE* C MW 
CLASSES PER TOR R 05/39 


1 fiEV/SE0 PER TDRR //6<*9 


REVISIONS 
DESCRIPTION 




ug_ 

jt 



.406 

REF 


I—.203 TYP 
, REF 


-p$) (P © 

USE WITH 1010311'KX 

-f©©©©.© 


-SEE. NOTE 3 


VIEW B'B 


INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED By MIL-D-70327 
R3ft R4 TO BE SELECTED PER ATP 1000286 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES, FROM 90K THRU IIOK OHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010695 
. R8(EXTERNAL FEEDBACK RESISTOR) TO BE SELECTED PER ATP '000286 
RANGE OF VALUES FROM 500 OHMS THRU 2K OHMS P£R PART NO. 1 010311 _ 

ONLY ONE RESISTOR SHALL BE SELECTED AND THE IART MO ^MB DASHI NO. SHALL 
BE MARKED ON THE COVER, AS SHOWN, PER ND 1002019 ft NDI002I22 TYPE 31 CLASS 1 
. IDENTIFY USING DRAWING NO., REVISION LETTER. SERIAL NO. AND 
MANUFACTURERS SYMBOL. PER MIL-STD-130 
. ENCAPSULATE WITH EPOXY PER ND 1002036, CURING CYCLE B 
. ASSEMBLY TO MEET REQUIREMENTS OF PS 1000286 

SOLDERING OF TERMINALS TO BE IN ACCORDANCE WITH MIL*5TD”440. ALL OTHER ELECTRICAL 
CONNECTIONS, SOLDER PER MIL-S-6872 WITH SN60 WRAP2. SOLDER PER QQ-S-571. 

. SOLDER COVER ASSEMBLY TO CASE PER MIL'S *6872A WITH SN50WRAP2 SOLDER 
PER QQ-S-571 

i. FINISH*. VINYL WASH PER MIL-C-I532B ANO ZINC CHROMATE PRIMER PER MIL-P-8585A 
PAINT BLACK SEMI GLOSS ENAMEL TTE'529 CLASS B. 

COLOR 27038 PER FEO STD 595 

3. R7 TO BE SELECTED PER ATP 10002 86 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 500 OHMS THRU lOKOHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO 1010694 
I. CENTER IDENTIFICATION PLATE OVER POTTING HOLE 

2 WINDING RESISTANCE FOR ACCEPTANCE TESTING*. (MEASURED INCH MAX FROM HEADER) 

terminals; 3 a 4 o.os ohm max 
5 a 6 0.05 OHM MAX 

3 INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A .007 GRAY FIBER SHEET 
PER MIL * 1 * 695A TYPE F, WITH A MINIMUM DIELECTRIC STRENGTH OF 

250VOLTS PER MIL 


REPLACES REV C WITH CHANGES 



SCHEMATIC 

IOOI622 


REF 



WIRING ASSEMBLY 

1001619 


REF 


A/R 

WIRE 

1006711-13 

AWG 30 


tl 

A/R 

GRAY 

FIBER SHEET 



NOTE 13 

10 

1 

RESISTOR 

1010694 

3 AT * 

NOTE 10 

9 

1 



1010695 

SAT 

NOTE 2. 

8 

1 



1010695 

SAT 

NOTE 2 

7 

1 

TRAN 

SFORMER 

1001623 



6 

1 

REACTOR ASSEMBLY 

1001620 



5 

1 

PRINTED CIRCUIT BOARD ASSEMBLY 

100161 8 


-i 

4 

1 

CASE 

ASSEMBLY 

1001647 



3 

1 

COVER ASSEMBLY 

10016 16 



2 

1 

PLATE* IDENTIFICATION 

1001543 


NOTE II 

l 

QTY 

REQO 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FINO 

NO 


LIST OF PARTS AND MATERIALS 








HEATER CURRENT 
AMPLIFIER 
ASSEMBLY 


M I T 

INSTWNMCirTATIOM 

LABORATORY 


S»CStf*Fr 

r - £4— 






UNIT WT. T COOE KJfNT 


8 


6 


5 


4 

























I Apollo C S N Specification 

PS-100028MI 

Class A Release 
TBRR 01266 
15 May 1963 


PROCUREMENT SPECIFICATION 


HEATER CURRENT AMPLIFIER 


Revision 

Letter 

TDRR 

No, 

Pages 

Revised 

Approvals 

Date 

MTT . 

WACA . 

B - 

02992 - 

Rev,replaces 
Rev. *k m with 
changee. * • 

'tJtk 


$ Sept. '63 

C 

03335 " 

Pages 1,3,5,10,1 
- f *1,11 •* 

' rjk 

( p 

26 Sept.*63 

B 

05156 

5«?&- 4 4Kl 

H oaxes, now 13.* 

1 4 


10 Dee. *63 

S 


Pages 4,8,9 & 10, 


jr 

2 June '64 









This specification consists of pages 
i to iv and 1 to 13 Inclusive* 


*/ 




' sx wht*r^ <•>«..•' 



Apollo GAN Specification 
PS-1000286-® 

5 Sept* 1963 


PROCUREMENT SPECIFICATION 
HEATER CURRENT AMPLIFIER 


Apollo GAN Specificati* 
PS-1000286-9 
$ O ep t* 19 6 3 
26 Sept. 1963 


HEATER CURRENT AMPLIFIER 


The purpose of this document is to establish the 
manufacturing and test requirements for procurement of 
the Heater Current Amplifier which is intended for use 
in the Apollo Guidance and Navigation Equipment program. 



MIT I) 


■WitlJ. ih-ki 

A /MOT ADDOnVAI ' * 


1. SCOPE 

1.1 SCOPE, This specification establishes the requirements for the 

procurement of the Heater Current Amplifier hereinafter called 
oq>lifier, 

2. APPLICABLE DOCUENTS 

2.1 The following documents of the issue in effect on the date of in¬ 

vitation for bids fonp a port of this specification to the extent 
specified herein. 

SPECIFICATIONS 

Military 

MIL-P-116 Preservation, Methods of 

MILE-17555 


NASA/MSC APPROVAL 


Apollo GAN 
ND-1002023 

ND-1002059 

ND-1015404 


ND-1002019 


Electronic end Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of - 


Procedure for Serialization of Components, 
Assemblies, etc,, for Apollo Guidance and 
Navigation equipment. 

Qualification'Specification, Magnetic 
Amplifiers 

General Specification, Configuration, 
Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment* * t 

Marking, General Specification for 


** r:*': 


; 





ii 


INCHES 

1 -a 1 J I 


I; 


O I £ 




) 


1 ‘ ^ 



PS-100028*# 


Class A Release 
TDRR 01266 
15 May 1963 


1WTURFMINT SPECIFICATION 
FOR 

HEATER CURRFNT AMPLIFIER 


Revision 

letter 

TDRR 

No. 

rages 

Revised 

Approvals 

Date 

. MIT. 


B 



m 

HB 

HI 

5 Sept. *63 

r* 

03335 

1,3,5,10,1" 

nu. 

■ 

Hi 

?'* "* 

n 

05156 

l* »»*»,. 88W 1?. 

m 

HI 

10 Pec. *63 

B 


Pages A,8,9 A 10, 


a 

2 June *6A 








This specification consists of pages 
i to iv and 1 to 13 inclusive. 




















Afo!!© (1 M Specification 
PS-1000286-B 
5 Sept. 1*>3 


HFATFR CURRFNT AMPLIFIER 


The purpose of this document is to establish the 
the^HMtpr'r^ and reouirewents for procurement of 
^ wpll li er which is intended for use 
m the Apollo Guidance and Navigation Fquipnent prograi 



ii 







PS-lUtMh'Bfc-D 
-S - 9e pt* 1963 
10 Dec. 1963 


PR0TUR!*CNT SPECIFICATION 

for 

HEATER CURRENT AMPUFIFR 


TABLE OF CONTENTS 

SECTION PATiF 

1 SCOTT . .. 1 

2 APPLICABLE PHCW-NTS. 1 

3 REQUIREMENTS. 2 

4 OUALITY ASSURANCE PROVISIONS. 7 

5 PREPARATION FOR DELIVERY. 12 

6 NOTFS. 12 









PS-1000286-e 
5 Sep t* l ‘ > 6 3 
26 Sap t. 1*>3 


mtvmwm specification 
HEATEP CURRENT AMP1IFIER 


STOPF. TMs specification establishes the requirements for the 
procurement of the Heater Current Amplifier hereinafter called 
amplifier. 

APP! ICABLE DnClM^NTS 


The following documents of the issue in effect an the date of in¬ 
vitation for bids form a part of this specification to the extent 
specified herein. 

SPECIFICATIONS 


Military 
Mil.-P-116 
MIE-E-17SS5 


Apollo G 6 N 
NO-1002023 

ND-1002059 

NP-101S404 


Preservation, Methods of 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of 


Procedure for Serialization of Components, 
Assemblies, etc., for Apollo Guidance and 
Navigation equipment. 

Qualification Specification, Magnetic 
Amplifiers 

General Specification, Configuration, 
Process and Ouality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment. 


NI>-1002019 


Marking, General Specification for 



P5-1UUUZH6-D 
10 Dec. 1963 


STANDARDS 


Federal 


2.2 


3. 


3.1 


3.2 


FIT)-STD-595 
Military 

MIL STD-130 


MIL-STu-202 


DRAWINGS 


Colors 


Identification Markin* of U.S. 
Military Property 

Test *tethods for electronic and 
F.lectrical Component Parts 


Apollo CM 

1000286 

1001620 

1001621 

1001623 


Heater Current Amplifier 
Reactor Assembly 

Core 6 Coil Assembly (Reactor Matched Pair) 
Core f» Coil Assembly (Transform^ Pwr) 


(Copies of specifications, standards, drawings, and publications 
reouired by suppliers in connection with specific procurement 
functions sltoulti he obtained from the procurinp activity or as 
directed by the contractin officer). 


CCNFUCTINC RIOtJIRFWNTS. In the event of conflict between the 
retirements of this specification and other specifications and 
drawinps cited herein, resolution must be obtained from the MIT 
APOLLO Management office via the purchaser. 


RFOIJIRFNtNTS 


The requirements of this specification are classified into two headings: 
General Requirements which are defined in parapraph 
3.2 ant) Performance and Product Characteristics which* 
are defined in parapraph 3.3. 

PFSTRIPTIPN. The unit shall be a mapnetic amplifier which provides 
a sipnal, proportional to the IHI heater current, used for monitoring 
telemetry and test points. 

GFNF.RAL RFOUIRFMSNTS 


3.2.1 Qualification Testinp . When specified by the purchaser, a representative 
sample of the amplifiers shall he manufactured usinp the methods and 
procedures proposed far the production lot. These shall he submitted 
to the NASA Inspector for-qualification tests at an activity desipnated 
in the contract or by the purchaser. These qualification tests are 
conducted to determine whether or not the amplifier? are be in* produced 
in compliance with the requirements of the contract, specification, and 
drawinps. Failure of the amplifiers to meet these requirements may result 
in disqualification of the supplier as determined by NASA or purchaser. 


2 



IO- 1UU\>£00-«J 

1963 

^ Oopt 1 |0 f)0c. 1963 

Further production of the item by the supplier prior to approval of 
the purchaser or the coaipletion of qualification tests shall he 
at the supplier's risk. Reaualification will be required at the 
discretion of NASA or the purchaser in the event that, (a) the 
supplier has modified the item, (b) the supplier has instituted 
a chanpe in the material used or in his processing, and (c) the 
specification requirements for the item have been amended or revised 
sufficiently to affect the character of the item. 

The qualification tests will be conducted in accordance with the 
procedures specified in Section 4, 

3.2.2 Requalification Testing, When specified by the procuring activity, 
the supplier shall submit one or more amplifiers to be selected 
from each production lot by the procurinp activity for submission 
to a designated testinp activity to determine compliance of the 
sample (s) with the requirements of the contract, specification, 
and drawinps. 

3.2.3 Materials and Construct ion. The materials used in fabricating the 
amplifiers shall be in strict accordance with the applicable 
drawinps and specifications referenced herein. Substitute materials 
shall be selected with such quality as to ensure that the equipment 
will meet the requirements of this specification and shall be subject 
to prior approval of the procuring activity. 

3.2.4 Weight. Dimensions. Finish, and Marking. The weight, dimensions, 
finish, and marking of the .unpliYier shall comply with the require¬ 
ments specified herein or on the applicable drawings. 

3.2.4.1 Weight . The weight of the amplifier shall not exceed 1.6 ounces. 

3.2.4.2 Finish. Finish shall be as specified on the applicable drawing. 


3.2.4.3 


Markinp Marking shall be in accordance with Mil .-STD-130.and 

ND-100201% and as specified m the applicable drawing. . 


Specification 


« un * 1 r 'T • iuiul itir at 1*w» 
"i* *ti*i frrti to re ^at»iv or. *-bc 


3.2.5 Serial Numbers. Fach amplifier identified by General Arrangement 
(or Assembly) Drawing shall be identified by a serial number 
assigned in accordance with Specification ND-1002023. 

3.2.6 Workmanship. The fabrication and finish of the amplifier, its assemblies, 
subassemblies, and parts he such as to produce a unit free from 

any defect that would affect proper functioning in service. 

3.2.7 Warranty. A warranty shall provide for the supplier to remedy by 
correction or replacement any* component or end item found to be 
defective in material or workmanship not later than six (6) booths 
after acceptance. 


The allowability of the cost of any such correction or replacement 
shall be determined as provided in the clauses of the appropriate 
contract entitled "Allowable Cost, Fixed Fee and Payment," and 
Inspection and Correction of Defects." 


3 



PS-1000286-J 

,r > OmU l ‘>fe 3 ' 


10 0 ec » 1 9 63 
2 June 1964 


3,2.8 Service I ife, 

3.2.8.1 Operating life. The amplifier design is intended to meet performance 
specifications for at least 20,000 hours of operation, excluding the 
supplier's test time of the completed unit. 

3.2.8.2 Shelf Life. The amplifier design is intended to have a shelf life 
of at feast 5 years, without operation, at ambient room temperature 
after final acceptance at the supplier's plant. 

3.3 PFRFPRMANTF AND PRODUCT CHARAfTFPISTIfS. The following requirements 

are stated to inform the supplier of specific characteristics and 
of the goals that were considered in the desipn. Inclusion of this 
information shall not he construed by the supplier as authorization 
to modify the design. 

If the design of any part is not completely specified by the con¬ 
tractual documents, the supplier may submit a suggested design 
document for approval which will support these retirements. 

If, in the opinion of the supplier, any design or testing shall 
impose undue time delay or expense, he shall so state, in detail, 
in a counter-proposal, substantiating all contributing factor* 
when submitting a bid, proposal, or change reouest. in connection 
tieh this specification. 

Requests for changes or deviations to this specification or to 
applicable drawings, specifications, publications, materials, or 
processes specified herein shall be accompanied by written 
justification. 

3.3.1 Functional Requirements. 

3.3.1.1 Winding Resistances. DC resistance of the windings shall be as 
specified on Apollo t $ N Drawings 1000286, 100162®, 1001621 and 1001623 

3.3.1.2 Dielectric Strength, The amplifier shall exhibit no evidence of 
breakdown when subjected to a 500V' rms voltage. 

3.3.1.3 Insulation Resistance. The insulation resistance of the amplifier 
shall he lo megohms minimum. 

3*3.1.4 Performance. Performance of the amplifier shall be as follows: 

3.3.1.4.1 Power Input. The amplifier shall operate with 50 ma maximum 
current from a 20 ♦ 2V rms, 3200 ♦ 32 cps source having the 
waveform characteristics specified in 4.2.2. . , 


PS-1 000286 -n 
10 Pec. 1963 


3.3.1.4.2 Cain . The unit shall provide an exit put of 0.0 ♦ 0.1 to 5.00 ♦ 0.25 
vSTwith a control current of 0 to 2 aarpeTea. The amplifier shall 
operate as specified after reaching thermal stability with the ambient 
temperature specified in 4.2.1, and apain after reachinp thermal stability 
with the ambient temperature of 150^ ♦ 5°F. When the ambient temperature 
is returned to that specified in 4.2.T and after thermal stabilization 
occurs, the amplifier shall apain operate as specified, fain shall 

he controlled by means of an external sealinp resistor. (Note: R3 (feed¬ 
back resistor] shall be in the same environment as the amplifier at 
ail times) 

3.3.1.4.3 Supply Voltage Sensitivity . The amplifier shall operate as specified 
herein with the ^200 cps source at any voltage between 18V raa 
and 22V raa. 


3.3.1.4.4 Output Ripple, flit put peak-to-peak ripple shall not exceed 50 m (0-10 kc). 

3.3.1.4.5 fVrtput Impedance . The output impedance shall be less th»i 1000 ohms. 

3.3.2 Fnvironmental Reouirements . The amplifier shall be capable of meetinp 

the reouirements of Specification NP-1002059. When a particular 
reouirement in Specification ND-1002059 includes the amplifier's 
capability of operation while Heine subiected to an environment, this 
shall he constiued to mean that an output of 2.5+ 0J.V shall be 
maintained under standard operating conditions as defined in 6.1.1. 


3*3.3 Pesipn Requirements . 

3.3.3.1 Tnterchanpeahi1ity . Unless otherwise specified, the amplifier and its 
component parts' snail be physically ami functionally interchanpeahle 
without selection or fittinp. 

3.3.3.2 Reliability . The amplifier shall be capable of operatinp a minimum of 
20,000 consecutive hixirs without maintenance under any combinations of 
conditions specified herein and shall have a maximun failure rate of 
0.5 failures per 1,000,000 hours. 

3.3.3.3 Radio Interference Suppression. The suppression of radio noise and 
interference sha11 be considered in the design of the amplifier. 

3.3.3.4 Flairmahle Materials. Materials which may he ipnited or cause an explosion 
sha11 not"he used for construction applications where sparking or arcing 


5 



PS-1000286-$ 

5 Sept. 15*63 

could cause ignition. Materials irfiich may inadvertently support 
combustion shall not be used. Flawnable impregnating, potting or 
embedding compounds, when enclosed in fire-resistance containers, 
shall be acceptable. 

3.3.3.5 Toxic Materials. Mateirals which produce harmful toxic effects 
during service usage shall not be used. Where a suitable.nontoxic 
material is not available, preventive measures shall be provided, 
subject to the approval of NASA. Materials which when ignited, 
produce toxic substances or vapors shall lie avoided whenever practicable. 

3.3.3.6 Unstable Materials . Materials which are unstable or become unstable 
to the extent that they emit or deposit aorrosive substances 
capable of causing corrosion or producing electrical leakage paths 
within an assembly under possible operating and storage conditions 
shall not be used during manufacture or recomnended for use 
during maintenance. 

3.3.3.7. Corrosion, Moisture, and Fungus-Resistant Materials. Materials 
shall be selected Tor noncorrosive and nonhvgroscopic character¬ 
istics and ability to resist the effects of corrosion, moisture 
ami fungus. Preference shall be given to materials with inherent 
fungus resistance rather than reliance upon the application of 
surface fungistatic or fungicidal treatments. 

3.3.3.8 Dissimilar Me t als. The use of dissimilar metals shall be avoided 
whenever practicable. Magnesiun shall not he used except with 
the prior approval of the procuring agency or when so called for 
on the applicable Apollo f. 5 N drawings. 


6 


PS-1000286-B 
5 Sept* l^bj 


4. QUALITY ASSURANCE PROVISIONS 

4.1 CFNFRAI. Unless otherwise specified herein, the supplier is 
responsible for the performance of all inspection requirements 
prior to submission for NASA inspection and acceptance. Except 
as otherwise specified, the supplier nay utilize his own 
facilities or any commercial laboratory acceptable to NASA. 

Inspection records of the examinations and tests shall he 

kept complete and available to NASA as specified in the contract 
or order. The supplier shall conform to Class 1 of Specification 
NO-1015404. 

4.1.1 Acceptance Tests. These tests shall be accomplished on each 
amplifier being submitted for acceptance under the contract. 
Acceptance test data on each unit accepted must accompany ship¬ 
ment to the purchaser. Acceptance tests shall he witnessed by 
the cognizant gove r nm ent inspector, a representative of the 
purchaser, or as the purchaser may direct in the procurement order. 
These tests are detailed in 4.2. Failure of the amplifier to 
oo^ly with these requirements shall result in rejection of the item. 

4.1.2 Qualification and Requalification Tests. Qialificaticn and 
rfequalification tests shall he accomplished at a NASA designated 
activity. These tests, as outlined in 4.3, shall be conducted after 
the award of the contract to determine that the production will meet 
all requirements of this specification. Acceptance shall be baaed 
on no defects in the amplifier. 

Failure of the amplifier to comply with these requirements shall 
result in the rejection of the lot or the cessation of production, 
as determined by the purchaser. 

4.2 ACCEPTANCF TESTS 

4.2.1 Test Conditions. Unless otherwise specified herein, the amplifier 
shall be subjected to tests under the following ambient conditions. 

(a) Temperature 25 ♦ 10* C 

(h) Relative Humidity Not more than 90% 

(c) Barometric Pressure 28 to 31 inches Ug. 

4.2.2 Test Power. The following electrical inputs, as measured at the 
Input of the unit oater test, are necessary for testing this item: 

(a) 20*2V ms, 3200*32 cps, square wave, 1.0 va maxima* power. 

The square wave shall have a rise time of 20seconds 
maximum Mid a balanced duty cycle within 5.0 percent. 

(b) Two 0 to 2 ampere dc current supplies 


7 


It lull 


4.2.3 


4.2.4 

4.2.5 


4.2.6 


4.2.7 


4.2.7.1 


PS-1000286-B 

44». D e e, 10 6 3 

2 June 1964 

Mechanical Inspection . A comprehensive inspection 
shall be made of the amplifier to determine the extent of 
compliance with the requirements of this specification and the 
applicable Apollo f 5 N dravinp specified in Section 2 and shall 
at least include determination on the followinp; 

(a) Size, dimension, tolerance, weipht, appearance and markinps, . 

(h) Adeauacy of materials, parts, and subassemblies; compliance 

with specific ratinps, and conformance to applicable specifications. 

(c) Finish, coatinps, construction, markinps, and nameplates, 
as applicable. 

(d) Kirinp, cablinp, weldinp, solderinp, color codinp and 
terminals, as applicable. 

(e) Workmanship and cleanup. 

PT Resistance . DT resistance shall be tested bv usinp method 303 of MII- 
Mi’— zvz and shall he as specified on Apollo C §, N Prawinp 1000286. 
1001620, 1001621, and 1001623. 

Dielectric Strength * Dielectric strenpth shall he checked by 
appivinp a 500V rms, 60 cps voltape between each terminal and 
the case and a 2f>0V rms. 60 cps (10PK source impedance) voltaee 
between the terminals specified in Table I. The leakape current 
shall not exceed 1.0 ma. This test shall he conducted in accordance 
with method 301 or MIb-STP-202. 


Tahle I. Dielectric Strength and Insulation Resistance 


Retween Terminals: 

Between Terminals: 

1 and 6 

6 and 3 

1 and 3 

6 and 8 

1 and 8 

8 and 3 


Ins til at ion Resistance. Insulation resistance shall be checked bv 
applyinp a 250 vdc voltape (current limited to 6 pamp) between each 
terminal and the case and between the terminals specified in Table I. 
The minimum acceptable resistance shall be 10 mepohms. This test 
shall be conducted in accordance with method 302 of MIb-STP-202. 

Performance. Performance of the amplifier shall he checked as 
follows. The test setup for these tests shall he as specified in 
Fipure 1. Unless otherwise specificd, switch S4 shall he in the 
open position. 

* nput * in P l,t current from the 20V rms. 3200 cps source 

snail he monitored at meter Ml durinp all of the Performance Tests. 

It shall not exceed 50 ma under any conditions. 


8 


R1 r R2 - 10 oh* t ♦lOI, 100W resistors 

R3 - Feedhack“resist or (Value as stamped on amplifier) 

Ml - 0*100 m thermocouple milliameter (Weston model, t>22 or equiv.) 
M2, M3 • 0 -tmw& a?wMr, ncrnrary 

»DC differential toltaeter, 0.05* accuracy tl aegoha aln 
Impedance) , 


Figure !• Test Setup 




4.2.7.2 


r»- FUIVBO-* 

10 0 ce » 10 * 3 ' 

2 June 1964 

Cain. With switch SI closed and switch S2 open, adjust the current indicated 
on neteT M2 to the values specified in Table II. The output voltape as 
measured at meter M4 shall he as specified in Table II. 

With SI open and S2 closed adiust the input current indicated on meter M3 
to the values specified in Table II. The output voltape as measured at M4 
shall be as specified in Table II. 

With SI closed and S2 closed, adjust both input currents (as indicated 
on *«2 and M3) to 0.5 ampere. The output voltape (M4) shall be 2,500* 

0.175 vdc. Readjust both input currents to 1.0 ampere. The output "" 
shall he 5.(HO.25 vdc. 

This test shall be performed three times, once in each of the following 
ambient temperature*, in the sequence indicat'd, after the amplifier 
and R3 (feedback resistor) attain thermal stability in the ambient 
temperature: 

(a) The temperature specified in 4.2.1 

(b) 150° ♦ 5°F 

(c) The temperature specified in 4.2.1 

Table II. Gain 


Input Current 
(amperes) 

(Xitput Voltage 
(vdc) 

0.00 

0.000*0.100 

0.50 

1.250*0.138 

1.00 

2.500*0.1*5 

1.50 

3.750*0.213 

2.00 

5.000*0.250 




4.2.7.3 Supply Voltare Sensitivity . With SI closed and S2 closed, hnd the 3200 cps 
supply adjusted to 1HV rms, adjust both input currents (M2 and ^*3) to 

0.5 ampere. The output voltape (M4) shall be 2.500*0.175 vdc. Readjust 
both inputs currents to 1.0 ampere. The output (M4j shall be 
5.000*0.250 vdc. 

Repeat the above test with the 3200 cps supply adjusted to 22V rms. 

(Xitput voltages shall again be as specified above. 

4.2.7.4 Qjtput Ripple . Connect a calibrated oscilloscope across meter M4. With 
51 closed and S2 open, vary the current indicated on M2 from 0.0 to 2.0 
amperes while monitoring the oscilloscope. The ac peak-tn-pcak ripple 
voltage present in the output shall not exceed 50 mv (0*10 kc). 

4.2.7.5 'Xitput Impedance . With SI closed and S2 open, adjust the current indicated 

on *<!z so that the output voltage (M4) is 5.00*0.2S. -4I.OO via. Tfean alaaa evltafc 
S4« The voltage at M4 shall not drop below 2.$ vdc. 


10 


PS-1000286-£ 

5 Sept. 1963 

4.3 OllAUFIfATICN ANT) RFOtJALIFIfATTnN Qualification and requalification 
tests shall be performed in accordance with Specification 

NP-1002059. When amplifier operation is included as a condition 
in a test in Specification NP-1002059, the amplifier shall be 
operated under standard operating conditions (see 6.1.1). The 
output shall be monitored during operation under standard operation 
conditions and shall be 2.5±0.1V at all tines. 

4.4 RFMABIfJTY. The reliability requireme n ts contained in Section 
3 of this specification are design objectives. Unless 
specifically called for in the procurement contract, it shall 
not be necessary for the supplier to demonstrate his compliance 
with the requirement. The supplier will furnish the purchaser 
or NASA such data as he nay have available for establishing the 
current reliability of these units. Additional data shall be 
accumulated to as great a degree as possible from the tests 
specified herein or any other tests the supplier may conduct 
which will tend to support or certify attainment of the 
reliability objectives specified. 


U 



PS-1000286-* 

5 Sent. 1963 
10 Deo.1963 

5. PREPARATION FOR DELIVERY 

5.1 PRESERVATION AND PACKAGING. The amplifier shall he preserved 
and packaged in accordance with Specification MIL-F-17555, 
level B, as specified in the contract or purchase order. 

5.1.1 Level B (Limited Military Packaging ). Level B packaging is that 
which vill afford adequate protection against damage during 
multiple domestic shipments, handling, and covered storage. 

5.1.1.1 Cleaning. Cleaning for Level B preservation and packaging shall 
be in accordance with method C-l of Specification MIL-P-116. 

5.1.1.2 Unit Protection. The amplifier shall he individually afforded 
unit protection in accordance with method III of Specification 
MIL-P-116. In addition, equi ent packaged for level B pro¬ 
tection shall be sealed agair water and dust by means of 
suitable wrapping. 

5.2 REPAIR PARTS. Repair parts shall have preservation and packaging 
per the applicable repair parts list and its packaging supplement. 

5.3 PACKING. The equipment shall be packed in accordance with Specifi¬ 
cation MIL-E-17S5S, level B. 

5.4 MARKING. In addition to any special marking required by the 

contract or order, the marking of unit, interior packages, and 
exterior shipping containers shall be in accordance with level 
B of Specification Mil -L-17555. 

6. NCTES 

6.1 DEFINITIONS 

6.1.1 Standard Operating Conditions. For the purposes specified in 

S.3.2 and 4.3, standard operating conditions shall he defined 
as follows: 

a) A power input of 20±2V rms, 3200t M cpe. fwitfc tfc* warn* form 
characteristics specified in 4.2.2) applied between terminals 

1 and 2. 

b) A feedback resistor f<see Figm* I >#onnaeted between n 
terminals 9 and 10.? Hi; 5 ?;• nr* . 

c) A 250Kt2 percent resistor and a dc differential voltmeter 
(0.05 percent accuracy) connected in parallel between terminals 
7 and 8. 

d) A 6.5 ampere dc aiYrent flowing through each mMllf, te rtrlnelf 
3 (♦) and 4 (-) and terminals 6 (♦) and 5 (•}. 

e) Unless otherwise specified in Specification NP-1002059, the 
test conditions listed in 4.2.1 shall apply. 


12 


PS-1000286-$ 
5 Sept. 1963 


NOTICE: When NASA drawings, specifications, and other data are 
used for any purpose other than in connection with a definitely 
related NASA procurement operation, NASA thereby incurs no 
responsibility nor any .obligation whatsoever, and the fact that 
NASA may have formulated, furnished, or in any way supplied the 
said drawings, specifications, or other data is not to be 
regarded by implication or otherwise as in any manner licensing the 
holder or any person or corporation, or conveying any right or permission 
to manufacture, use or sell any patented invention that may in any 
way be related thereto. 


13 



irWW 


i • ■* 

= FM ■»' 

► V ..i 

%• , . ,1 

'■A' 

* 0 


rj - 

'C 


1 


-SUMS 

"zm 

-m'-h- 

**»*«i# 


f! 0 


r 

i '1 

1 

j 

j : 


0 1 



T 

,50 Mir 

t 


r 

.406 

REF 

_L . 


®-. 


*+.04 , 

5 -.02 1 


—] i—.203 TYP 

■ ^ REF 

t it (M * i* 

-\f> 0 © 01 

USE WITH 1010311 

—© ©00© 


view B _ B 



SEE NOTE 3 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D'70327 

2. R3 S R4 TO BE SELECTED PER ATP 1000286 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES, FROM 90K THRU IIOKOHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010695 

3. R8 (EXTERNAL FEEDBACK RESISTOR) TO BE SELECTED PER ATP 1000286 
RANGE OF VALUES FROM 500 OHMS THRU 2K OHMS PER PART NO. 1010311 

ONLY ONE RESISTOR SHALL BE SELECTED AND THE PART NO. ANft DASH NO. SHALL 
BE MARKED ON THE COVER, AS SHOWN, PER NO 1002019 d ND 1002122 TYPE H CLASS 1 

4 . IDENTIFY USING DRAWING NO., RE VI SION LETTER, SERIAL NO. AND 
MANUFACTURERS SYMBOL. PER MIL-STD* 130 

5. ENCAPSULATE WITH EPOXY PER ND 1002036, CUR ING CYCLE B 

6. ASSEMBLY TO MEET REQUIREMENTS OF PS 1000286 

7. SOLDERING OF TERMINALS TO BE IN ACCORDANCE WITH Mll*5TD-440. ALL OTHER ELECTRICAL 
CONNECTIONS, SOLDER PER MIL-S-6872 WITH SN60 WRAP2 SOLDER PER QQ-S-571. 

8. SOLDER COVER ASSEMBLY TO CASE PER MIL'S *6872 A WITH SN50WRAP2 SOLDER 
PER QQ-S-571 

9. FINISH*. VINYL WASH PER MIL*C-I5328 AND ZINC CHROMATE PRIMER PER MIL-P-8585A 

PAINT BLACK SEMI GLOSS ENAMEL TT-E'529 CLASS B. 

COLOR 27038 PER FED STD 595 

10. R7 TO BE SELECTED PER ATP 1000286 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 500 OHMS THRU lOKOHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO 1010694 

11. CENTER IDENTIFICATION PLATE OVER POTTING HOLE 

12. WINDING RESISTANCE FOR ACCEPTANCE TEST ING*. (MEASURED /& INCH MAX FROM HEADER) 

TERMINALS; 38 4 0.05 OHM MAX 

5 ft 6 0.05 OHM MAX 

13. INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A .007 GRAY FIBER SHEET 
PER MIL-1- 695A TYPE F, WITH A MINIMUM DIELECTRIC STRENGTH OF 

250 VOLTS PER MIL 

14. FOR THE 1000286*000 ASSEMBLY THE TYPE I REQUIREMENTS OF THE PS AND ATP 
SHALL APPLY IN NOTES 2,3,* AND 10 OF THIS DRAWING. 

15. FOR THE 1000286-011 ASSEMBLY THE TYPE H REQUIREMENTS OF THE PS AND ATP 
SHALL APPLY IN NOTES *,3,6 AND 10 OF THIS DRAWING. 


f 


' i if I 







































APOLLO G&N Specification 
PS 1000286 F 


PROCUREMENT SPECIFICATION 
HEATER CURRENT AMPLIFIER 


1. SCOPE 

1.1 SCOPE. This specification establishes the requirements for the procurement of 
the Heater Current Amplifier hereinafter called amplifier. 

1.2 CLASSIFICATION. The requirements for the equipment covered by this specification 
shall be classified as follows. Unless identified by the respective type, all requirements of 
this specification are applicable to all types. 

a. Type I: The requirements for Part Number 1000286-000 shall be designated 
as Type I in this specification and identified as PS1000286-000. 

b. Type II: The requirements for Part Number 1000286-011 shall be designated 
as Type II in this specification and identified as PS1000286-011. 

2. APPLICABLE DOCUMENTS 

2. l Hie following documents of the Issue in effect on the date of invitation for bids 
form a part of this specification to the extent specified herein. 


SPECIFICATIONS 

Military 

MIL-P-116 

MIL-E-17555 

APOLLO G&N 
ND-1002023 

NI>-1002059 
ND-1015404 


Preservation, Methods of 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of 


Procedure for Serialization of Components, 
Assemblies, etc., for APOLLO Guidance and 
Navigation Equipment. 

Qualification Specification, Magnetic Amplifiers 

General Specification, Configuration, Process and 
Quality Control Requirements for Suppliers of High 
Reliability Articles for Use in Spacecraft and 
Supporting Equipment 


ND-1002019 


Marking, General Specification for 



Apollo C G N Specification 
PS-1000286-* 

•f 

». v-t, . i*»-5 


3.2.8 Scn f ice I ife. 

3 2 8 1 Operating l ife. The amplifier design is intended to meet performance 

* speciI legations’ foT at least 20,000 hours of operation, excluding the 

supplier’s test time of the completed unit. 

3282 Shelf life. The amplifier design is intended to have a shelf life 
of at lea's? 5 years, without operation, at ambient room temperature 
after final acceptance at the supplier’s plant. 

3.3 ITProRMANTT AMP PRPDirr fHAPAfTFPlSTTrS. Tlx? following requirements 

are stated to inform the supplier of specific characteristics and 
of the goals that were considered in the design. Inclusion of this 
information shall not he construed hy the supplier as authorization 
to modify the desip,n. 

If the design of any part is not complexly specified by the con¬ 
tractual documents, the supplier may submit a suggested design 
doci**ent for approval which will support these reouirements. 

Tf, in the opinion of the supplier, any dcsipn or testing shall 
impose undue time delay or expense, he shall so state, in detail, 
in a counter-proposal, substantiating all contributing factors 
when submitting a bid, proposal, or change reouest. in connection 
tieh this specification. 

Reouests for changes or deviations to this specification or to 
applicable drawings, specifications, publications, materials, or 
processes specified herein shall be accompanied by written 
just if teat ion. 

3.3.1 functiona1 Pcauirement s. 

3.- l.l Winding Resistances. DC resistance, of the vimlings shall be as 

srcc { He;! on ApoHe P f« N Drawings 10002&, 100162©, 1001631 and 1001623.* 

3.3.1.2 Pielectric Strength. The amplifier shall exhibit no * %, idence of t * 

! real clow vi.cn sul Tect ed to a 500Y rms voltage 

3.3.1.3 Insulation Resistance. The insulation resistance of the amplifier 
slial 1 \ c lb megohms ninimur, 

3.’. 1.1 ’’erferrv.ncc. Performance of the aryliiirr shall he as follows: 

t.l bowoi input. Tie amplifier shall opern*, with SO ma mnxirtn 

uurT7TV T r or n 2*' ♦ H rms. 3200 ♦ ; 1 - source (Type I) or a 20*4,-2V rms, 
3200 ± 32 eps source (Type II) having the waveform characteristic# specified In 
4.2.2. 



Apollo f f, N Specification 
PS-10002h6-F 


3.3.1.4.2 Cain . The unit shall provide an output of 0.0 ♦ 0.1 to 5.00 ♦ 0.2S 
vtTTVith a control current of 0 to 2 ampere*. The amplifier shall 
operate as specified after reaching therm’ stability with the arhient 
tcmjxjrature specified in 4.2.1, and apain after reacl.inp thermal stability 
Kith the ambient temperature of 150° ♦ S°F. ! hen the ambient temperature 
is returned to that specified in 4.2.T and after thermal stabilization 
occurs, the amplifier shall apain operate as specified, fain shall 
he controlled by means of an external sen Imp resistor. (Note: P3 [feed- 
bad resisted shall be in the same environment as tlie amplifier at 
all times) 


3.3.1.4.3 supply Voltarc Scnsitivitv. The amplifier shall operate as specified 

herein with the 3?00 epa source at any voltage between 18V rms 
and 22V rms /Type I) or 24V rms (Type II). 


3.3.1.4.4 f\itput Rirrle . (\itput pcak-to-peak ripple shall not exceed SO mv ((’-10 kc). 

3.3.1.4. S nut put I rrpedance » The output impedance shall he less than 1000 ohms. 

3.3.2 knvironmortal ncunirencnis . The amplifier shall le capable of meet inr 

the rcouircmcnts of £pec l'fication NO-1 (’02059. vben a particular 
reouirement in Specification Nf>-l(’O2059 includes the amplifier's- 
capability of operation while bcinn suhiocted to an ervir^wnt, this 
shall be construed to mean that an output 4 of 2.5* 0.1V shall be 
maintained under standard operating conditions as defined in 6.1.1. 


3.3.3 


3.3.3.1 


3.3.3.2 


3.3.3.3 

3.3.3.4 


Pesipn Pcouiremcnts. 


Tntcrchnnpeahilitv. !>nlcss otherwise specified, the amplifier and its 
component jarts sha11 be physically and functionally intcrchanpcahle 
without selection or fit tine. 

n eliahilitv. The amplifier shall he capable of operatinp a minimum of 
20,i’f’O consecutive hours without maintenance under any combinations of 
conditions specified herein and shall have a raAimum failure rate of 
0.5 failures per 1,000,000 hours. 

Padie Interference Suppression. The suppression of radio no4sc apd 
interference shall be considered in the desipn of the amplifier. 

Ftamable "aterials. 'Materials which ray be ipnited or cause an explosion 
shall not !c uscxT for cpnstruction applications where sparkinp or arcinp 


5 


J 



Apollo f f, N Specification 
PS-100028h-F 


PFAFITY ASSI’PANCF PROVISIONS 

(TNTf'A! . Unless otherwise specified herein, the supplier is 
responsible for the performance of all inspection requirements 
prior to submission for NASA inspection and acceptance, hxcept 
as othervise specified, the supplier may utilize his own >•« 

facilities or any commercial laboratory acceptable to NASA. 

Inspection records of the examin; tions and tests shall he 
kept complete and available to NASA as specified in the contract 
or order. The supplier shall conform to <lass 1 of Specification 
NP-101S104. 

Acceptance Tests. These tests shall be accompli shed* on each 
amplifier beinp submitted for acceptance under the contract. 
Acceptance test data on each unit accepted must accompany ship- * 
went to the purchaser. Acceptance tests shall be witnessed by 
the cognizant government inspector, a representative of the * * 

purchaser, or as the purchaser may direct in the procurement order. 
These tests are detailed in 4.2. Failure of the amplifier to 
comply with these requirements shall result in rejection of the item. 

fXialif ication and kcquaiification test^. Dual ification and 
^qualification tests sballbeavcbmplisbeo at a NASA designated 
activity. These tests, as outlined in shall be conducted after 
the award of the contract to determine that the production will meet 
all requirements of this specification. Acceptance shall be based 
on no defects in the amplifier. , 

Failure of the amplifier to comply with tbe^e requirements shall 
result in the rejection of the lot or the cessation of production, 
as determined by the purchaser. 

AfrTPT.ANTF TF.STS 

Test Fonditions. Italass otherwise specified herein, the amplifier 
shall he suljected to tests under the following ambient conditions. 


(a) 

Temperature 

2S ♦ 10° 

r 

(b) 

Relative Humidity 

Not more 

than 901 

1c) 

Barometric Pressure 

28 to 51 

inches iig 


Test Power. The following electrical inputs, as measured at the 
lupuPoTThe unit undeT test, arc necessary for testing this itat: 

(a) 20±2V nqs, (Type I), a»*4, -2V rm# (Type II) 3200*82 epe, aquari wave 
1.0 va maximum power. Hie square wave shall have a rise time of 26 fi 
seconds maximum and a balanced duty cycle within 5.0 percent. 

(b) Two 0 to 2 ampere de current supplier. 


£ 



Apollo C G \ ^pccification 
PS-100028* -F 


v isi::il and Vccl.anical Inspect ior, . A comprehensive inspect ion 
shall Vc made of the ary'nfiertc clctcrrinc the extent of 
corpliance Kith the requirements of this specification and the 
applical lc Apollo C G N dravinp specified in Section 2 and shall 
at least include determination on tie follovinp; 

(a) Size, dimension, tolerance, weipht, appearance and markinrs* 

(I) Adcouacy of materials, parts, and subassemhlies; compliance 

with specific ratinps, and conformance to applicable specifications. 

(c) Finish, coatinps, construction, rarlinps, and nameplates, 
as applicable. 

(d) Kirinp, cahlinp, weldinp, solderinp, color codinp and 
terminals, as applicable. 

(c) Workmanship and cleanup. 

T K' Resistance. PT resistance shall le tested hv usinp method 303 of M 4I - 
nm! shall l>c as specified on Apollo f f, N PraKinn 1000286, 
10U1620, 1001621, ami 1001623. 

Pielectric Strcnrth . Pielectric strenpth shall bp checked hv 
applvinp a ^OoV rms, 60 cps voltage between each terminal and 
tie case and a 200V rms. 60 cps ( loot: 'source irpedance) voltape 
between the terminals specified in Table I. The leal ape current 
shall rot exceed l.o ma. This test shall he conducted in accordance 
with method 301 or MI! -STP-202. 


Table 1. Pielectric * ; trcnt»tb and Insulation resistance 


between Terminals: 

Pet ween Terminals: 

I am 1 <' 

( anil 3 

/I and 3 

6 ami 8 

1 and 8 

8 am! 3 


Insulation resistance. Insulation resistance shall lc checked by 
applvinp a 2*0 vile volt ape (current limited to 6 |*amp) between each 
terminal .am! the case am! between the terminals specified in T.ahle I. 
The minimum acceptable resistance shall be 10 mcpolims. This test 
shall he conducted in accordance with method 302 of ‘’H.-STP-2P2. 

Pcrforrarcc. Performance of the amplifier shall he checked as 
f 1 c 11 ows. the test setup for these tests shall he as specified in 
Tipurc 1. l'nless otherwise specifiec!, switch S4 shall he in the 
ofon position. 

Rover Input . The input current from the 2P\’ rms (Type I) or 21V rra® 
(Type II) 3200 ope source shall be monitored at meter Ml during all of the 
Performance Tests. It shall not exceed 50 ma under any conditions. 


8 


j 



Apollo G & N Spec i f icat r on 
P5-f0D02&6-T 


20±2V mis (Typ I) 

20+4, -2V m>fi (Type II) 
3?P0H? cpft 


f f 



ni t . = 1(1 oilr, -10* , 1001. re‘*’stors 

T, 3* = ! mil mc).“ resistor f'nlue n< *t«Trpci! on nrpliUeri 

\<] - p. loo m tl crrocouplc ni 11 iareter (V.c^^r ’’txio!, (22 or couiv.! 

»V*. •- o.?-*"p*r nr^’-^'-y 

M4* -DC differential voltmeter, 0.05< accuracy (1 megohm min. Input 

Impedance) 


Figure 1. Test Setup 


9 




j. 




Apollo COM S?ooifjcntjen 
P5-10G286-F 


4.2.7.2 fain. Kith switch SI closed and switch S2 open, adiust the current indicated 
or rcter M2 to the values specified in Table II. The output voltage as 
treasured at meter M4 shall be as specified in Table IT. 

With SI open and S2 closed adiust the input current indicated on meter M3 . 
to the values specified in Table II. The output voltape as measured at M4 
sliall be as specified in Table II. 

Kith SI closed and S2 closed, adjust both input currents (as’indicated 
on M2 and M3) to 0.5 ampere. The cutput voltape (M4) sliall be 2,500* 

0.175 vdc. Readjust both input currents to 1.0 ampere. The output 
shall be 5.0*0,25 vdc. 

This teatAall be performed three times, once in each of the following 
ambient temperatures,.in the sequence indicated, after the amplifier 
and R3 (feedback resistor) attain thermal stability in the ambient 
temperature: 

(a) The temperature specified in 4.2.1 
(h) 150° ♦ 5°T 

(c) The temperature specified in 4.2.1 


Table II. Gain 



4.2.7.3 Supply VoItare Sensitivity. With SI closed and S2 closed, hod the 3200 cps 
supply adlusted to 1»V Tms, adjust both input currents (M2 and *5) to 

0.£ ampere. The output voltape (M4) shall be 2.500*0.175 vdc. Readjust 
both inputs currents-to 1.0 ampere. The output (M4T shall he 
5.000*0.250 vdc. 

Repeat the above test with the 3200 cps supply adjusted to 22V rms (Type I) ;■ 
or* £4V ' rms (Type H). Oatpat voltages shall agaia be as specified above. 

4.2.7.4 Output Ripple. Connect a calibrated oscilloscope across meter Ml, With 

closed and S2 open, vary the current indicated on 7*2 from 0.0 to 2.0 
amperes while monitorinp the oscilloscope. The ac pcak«*-»-peak ripple 
voltape present in the output shall not exceed 50 mv (0-10 kc)<* 

4.2.7.5 Output Impedance. With SI closed and S2 open, adiust the current indicated 

on so thnf the output voltape (M4) is 5.00*0.25, -0.00 vie. flMB aloaa Mdtsh 
S4. The voltape at M4 shall not drop below 2.S vdc. 

10 


•I 



PREPARATION POR nTUVFRY 


Apol i o C f, V Spec i f: cat i on 
PS-1000286-? 


5. 

$.1 


PRLSTPVATION AMP PAfkACTNC. T)»e amplifier shall he preserved 
and packaged in‘accordance with Specification Mil.-P-17555, 
level B, as specified in the contract or purchase order. 


5.1.1 . Level B flimited Military Packaging). Level B packaging is tlfet 

which v i I I nffV>r<l adequate protect ion against damage during 
multiple domestic shipments, handling, and covered storage, 

5.1.1.1 Cleaning. Cleaning for level B preservation and packaging shall 

be in accordance with method C-l of Specification Mil.-P-116. 

'# 

5.1.1.2 Unit Protection. The amplifier shall he individually afforded 

unit protection in accordance with method III of Specification 
MfL-P-U6. In addition, eouipment packaged for level B pro. 
tection shall be sealed against water and dust by means of 
suitable wrapping. r 

5.2 RFPAIR PARTS. Repair parts shall have preservation and packaging 
per the applicable repair parts list and its packaging supplement. 

5.3 PACKING. The eouipment shall be packed in accordance with Specifi* 
cation Mff-f-17555’, level B. 

5.4 MARKING. In addition to any special marking, required by the 

contract or order, the marking of unit, interior packages, and 
exterior shipping containers shall be in accordance with level 
B of Specification Mil -I -17555• *#■ 

6, ' NOTTS ' 

. 6.1 WFINITIONS 


6.1.1 Standard Operating Conditions. For the purposes specified in 
3.3.2 and 4.3, standard operating conditions shall be defined 
as follows: 


a) A power input of 20* 2V rms, (Type I) or 20*4, -2V rma (Type II) 3200*32 epa 
(with the wave form oharaoteiiatles epeclfied la 4.2.2) applied between tana Inals 

1 and 2,•. 

*. ■ 

b) A feedback -csisto' fame Figure I )coaneot#d betweea c ”* 

terminals 9 and 10. .. 

c) A 250k't2 percent resistor and a dc differential voltmeter 
(0.05 percent accuracy) connected in parallel between terminals 
7 and 8. 

d) A B.S ampere dc .current flowing through each winding, terminals 
3 (♦) and 4 (-) anil terminals 6 (♦) and 5 (-}• 

e) Unless otherwise specified,.;in Specification VP-1002059, the 

test conditions listed in 4.2.1 <hall applv. * 


n 




9 83 0001 


REVISIONS 

DESCRIPTION 


DATE I APPROVAL 


0 - > HI 1201/ ±10% RMS 

13200 CPS —. 

© - ” AV£ 









































i 


Apollo G 5 N Specification 
PS-1000286 
15 May 1965 
Class B Release 
TDRR CiX.UU 


PROCUREMENT SPECIFICATION 
FOR 

WATER CURRENT AMPLIFIER (MA20A-1) 


Record of Revisions 


Revision 

Letter 

TDRR 

No. 

Pages 

Revised 

Approval. 

MIT NASA 

DATE 






i -i 


















I 



This specification consists of Pgge i to iii and 
1 to S inclusive* 


Apollo GAB Specification 
PS-1000286 
15 Kay 1963 



SATURABLE REACTOR 
HEATER CURRENT AMPLIFIER (MA20A-1) 


2 . 


2.1 


The purpose of this document is to establish the manufacturing 
\ requirement8 fop Procurement. The Heater Current Amplifier 
(KA20A-1) is Intended for use in the Apollo Guidance and Navigation 
Equipment program. 6 


MIT 





Apollo G 6 N Specification 

PS-1000286 

15 May 1963 


PROCUREMENT SPECIFICATION 
WATER CURRENT AMPLIFIER (MA20A-1) 


SCOPE 

This specification establishes the requirements for the p roc u rement 
of the Heater Current Amplifier (MA20A-1), hereinafter called the 
smplifer. 

APPLICABLE DOCUMENTS 

The following documents of the issue in effect on the date of 
invitation for bids form a part of this specification to the extent 
specified herein. 

SPECIFICATIONS 

Military 


MIL-T-27 


Transformers and Inductors 


MIL-P-116 

MIL-I-16910 

MIL-P-17555 

i 

Apollo GAN 
ND-101540# 


STANDARDS 

' Military 

MIL-STD-810 


DRAWINGS 


Preservation, Methods of 

Interference Measurement, Radio, Methods 
and Limits, 14 Kilocycles to 1000 
Megacycles 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of 


General Specification, Configuration, Pro¬ 
cess and CHiality Control Requirements for 
Suppliers of High Reliability Articles for 
use in Spacecraft and Supporting Equipment. 


Environmental Test Methods for Aero¬ 
space and Ground Equipment 


NASA/MSC APPROVAL 


NASA 


1010039 

1000286 


Apollo IMJ Temperature Control System, 
Scyematic 

Heater Current Amplifier (MA20A-1) 


11 


1 


























































Apollo C|N Specification 
PS-1000287 -A 
i > Vav i*)v.3 

Clast B Release 
TDRR O HUU 
15 May 1963 



Apollo C|N Specification 
PS-1000287 
IS May 1963 


Apollo G|N Specification 

PS-1000287 

15 May 1963 


/ 

PROCUREMENT SPECIFICATION 


IMU BLOWER CURRENT SENSOR (MA 2SA-1) 


PROCUREMENT SPECIFICATION 
FOR 

IMU BLOWER CURRENT SENSOR (MA2SA-1) 


IMU PLANER CURRENT SENSOR (MA2SA-1) 


| 1. SCOPE 

1.1 SCOPE. This specification establishes the requirements for the pro- 

i curement of the IMU Blower Current Sensor (MA25A-1) hereinafter 

I called sensor. 

I 2. APPLICABLE DOCUMENTS 


Record of Revisions 


revision 

Letter 

TDRR 

No. 

Pages 

Revised 

Approvals 

DATE 

MIT NASA 

A 

01734 

Page 5 







I 












The purpose of this docunent is to establish the manufacturing and 
test requirements for procurement. The IMU Blower Current Sensor 
(MA2SA-1) is intended for use in the Apollo Guidance and Navigation 
Equipment program. 


% 


This specification consists of Page i to iii and I 

I to 9 inclusive# | 


hit i^wimnrrnN rAimfro 

jZvLA/ r///a 

NASA/MST APPROVAL'/ 


i 

2*1 

The following docunents of the issue in effect on the date of invitation 
for bids form a part of this specification to the extent specified 
herein. 

» 

i 


SPECIFICATIONS 


l 


Military 


i 

i 


MIL-T-27 

Transformers and Inductors (Audio t Power, 
and Pulse) 

> 

1 


MIL-P-116 

Preservation, Methods of 

i 

f 


MIL-I-16910 

Interference Measurement, Radio, Methods 
and Limits, 14 Kilocycles to 1000 Megacycles 

f 


MIL-E-175S5 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of 



Apollo GIN 




4 ND-1002023 

Procedure for Serialization of Components, 
Assemblies, etc., for Apollo Guidance and 
Navigation Equipment 



ND-101S404 

General Specification, Configuration, Pro¬ 
cess and Quality Control Requirements for 
Suppliers of High Reliability Articles for 

Use in Spacecraft and Supporting Equipment. 


| 


i 

I 


I 


ii 


1 





7 


6 



A *1 



A*J 


VIEW WITH COVER 
REMOVED 


' : Moresi 

' y ‘ ~ L 

t 

a 

A. 

S 

e. 

7. 

a. 


*3 TV BE SELECTED PE /? ATP /000237 AFTEP /U/T/AL eUCAPSULAT/O// 

ftAMZE OF VALUES, FPOM 3* TUPU +KOUMS ///STEPS OF 2JO//MS 

n \>0 FES/STOPS MAY ME USED TO GET A/EEDED. VALUE* PEP PAPT NO* /010363 


IDENT\FY US\NG DRAW\NG NO.,REVISION LETTER, SERIAL UO. AND 

MANUFACTURER* SYMBOL PER MIL -STD - ISO 

ENC AJPSjPL AT E WITH EPOXY PER ND10020SG, CURING CYCLE B 

ASSEMBLY TO MEET ALL REQUIREMENT* OF PS IOOOEB7 

USE SNGO SOLDER PER QQ.-S- 57 I FOR ALL ELECTRICAL CONNECTORS 

USE SN50 SOLDER PER QQ-S-S7\ TO SOLDER COVER ASSV. TO CASE 

Winding res\stancr for acceptance testing between terminals 142-01 omSMAx 

FINISH * VINYL WASH AND Z.INC CHROMATE PRIMER PER MIL-F-GBBS TYPE \ 




























































Apollo CM Specification 

PS-1000287 

15 May 1963 



PROCUREMENT SPECIFICATION 
IMU BLOWER CURRENT SENSOR (MA 25A-1) 


SCOPE 

SCOPE. This specification establishes the requirements for tie pro¬ 
curement of the IMU Blower Current Sensor (MA25A-1) hereinafter 
called sensor. 

APPLICABLE nOClM-NTS 

The following documents of the issue in effect on the date of invitation 
for bids form a part of this specification to the extent specified 
herein. 

SPECIFICATIONS 

Military 

MIL-T-27 Transformers and Inductors (Audio, Power, 

and Pulse) 

MIL-P-116 Preservation Methods of 

MIL-I-16910 Interference Measurement, Radio, Methods 

and Limits, 14 Kilocycles to 1000 Megacycles 

MIL-E-175S5 Electronic and Electrical Equipment and 

Associated Repair Parts, Preparation for 
Delivery of 

Apollo GAN 

i ND-1002023 Procedure for Serialization of Components, 

Assemblies, etc., for Apollo Guidance and 
Navigation Equipment 

ND-1015404 General Specification, Configuration, Pro¬ 

cess and Ouality Control Requirements for. 
Suppliers of High Reliability Articles for 
Use in Spacecraft and Supporting Equipment. 


REV. b 



















































7 


6 




VIEW WITH COVER 
REMOVED 


t/oresz 


R3 TO BE SELECTED PEA ATP W00Z87 AFTER /W/T/PL eNCAPSULAT/O/J 
RA/&E OF YAU/ES, FROM 3K TNRU +P 0WmS /U STEPS OF 

TWO EES/STOPS MAY ME USED TO GET WEEDED. YAUJE.- PEP PART ML /0/06 $3 
IDENTIFY l)S\NS DRAW\NG NO.,REVISION LETTER, SERIAL. WO. AMD 
MANUFACTURERS SYMBOL PER M\L-STD-\SO 
ENCAPSULATE. WITH EPOXY PER ND10020SC ,CUR\NG CYCLE B 
ASSEMBLY TO MEET ALL REQUIREMENTS OF PS IOOOEB7’ 

SOLDER/NG OF ELECTR/CAL CONNECT/ONS TO ME. IN ACCORDANCE Pl/TN M/L‘ STD-44-0 
W/TR SN6QWARP& SOLDER REP QQ-S-57/ 

SOLDER COYER ASSEMBLY TO CASE PEP M/L-S- 6&7&A 
W/TN SN50WARPS SOLDER PER QQ->5 ~ 57/ 
tN/UD/MQ RES/STANCE TOR ACCEPTANCE. T1EST/NGI 
TERM/NALS / f 2 0.1 ON M MAX. 

R/N/SN: Y/NYL wash RER M/E- C-/53ZB and Z/NC C**°^ r£ L.£ R J n AAA A 

PER MIL - D - 8585A y PA/NT 3LACP SEN//- GLOSS ENAMEL TT-E- S&9 CLASS O 
COLOR 27036 PER FED. STD 59S 

INTERPRET DRAWING IN ACCORDANCE W/TN STANDARDS 
PRESCRIBED BY NHL-D-703Z7 

, INSULATE ELECTP/CAL COMPONENTS PROM CASE W/TN A 
.007 GRAY F/BER SNEET RER M/L-I- 69SA TYPE P 
R/TM A M/N/MUM D/ELECTR/C STRENGTH OP £SO YOLTS PER M/L 

CENTER 1DENT/P/CAT/ON PLATE OYER POTT/NG NOLE 


♦ 



VTT] 


































Apollo G5N Specification 
PS-1000287- C 
ij M nv ivH'O 

Class B Release 
TDRR O\X(0¥ 

15 May 1963 



Apollo CM Specification 

PS-1000287 

IS May 1963 


PROCUREMENT SPECIFICATION 
FOR 

IMU BLOWER CURRENT SENSOR (MA2SA-1) 


IMU Pi0l& CURRENT SENSOR (MA2SA-1) 






i 

II 


Record of Revisions 


Revision 

TDRR 

Pages 

AoDTOvals ] 


Letter 

No. 

Revised 

MIT 

NASA 

DATE 

1 

01734 

Page 5 

u/M 



B 

02312 

Pare i and 4 

hift /A 

r 

31 July 63' 

C 

<£>3/ff 

Rev* "C"replaced bj 
Rev. D witn changes. 

tjt 

17 Sept'63 







The purpose of this docu we n t is to establish the manufacturing and 
test requirements for procurement • The 1MJ Blower Current Sensor 
(MA2SA-1) is intended for use in the Apollo Q iidan c e and Navigation 
Equipment program* 


This specification consist* of Page i to iii and 
I to 9 inclusive. 


RGl/. “C* REPLACE Bi XEt 

wirrt cttAVGrEs, 


a 



NASA/MSC APPP^vaT * ' 


wm, 


Apollo CM Spec if initial 

PS-1000287 

15 May 1963 

’ I 


PROCURE^NT SPECIFICATION 
IMU BLOWER CURRENT SENSOR (MA 25A-1) 


1. SCOPE 

1.1 SCOPE, This specification establishes the requirements for the pro¬ 

curement of the IMU Blower Current Sensor (MA2SA-1) hereinafter 
called sensor. 

2. APPLICABLE DOCIM-NTS 

2.1 The following docunents of the issue in effect on the date of invitation 

for bids form s part of this specification to the extent specified 
herein* 

SPECIFICATIONS 

Military * 

MIL-T-27 


MIL-P-116 
MIL-I-16910 

MIL-E-1755S 

Apollo CM 
ND-1002023 

ND-101S404 


Transformers and Inductors (Audio, Power, 
and Pulse) 

Preservation, Methods of 

Interference Measurement, Radio, Methods 
and Limits, 14 Kilocycles to 1000 Megacycles 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of 


Procedure for Serialisation of Components t; 
Assemblies, etc,, for Apollo Qi idan ce and 
Navigation Equipment 

General Specification, Configuration, Pro 
cess and Ouality Control Requirements for 
Suppliers of High Reliability Articles for 
Use in Spacecraft and Supporting Equijmani. 


ii 


■A 


I 





replaces rev a with changes 

AND UPGRADED TO CLASS A, acT 

PER TDRR 03570. ___ 

' / wl^/aco rc/i ro*A os/53 '*-*■*§ 
' REVISED PER TDRR 06073 


2 I 4 

fit 


Vielh/ 3~3 



VIEW WITH COVER 
REMOVEO 



1 ®l~ 


4.40NC-2A REF 



56a I 

t.OJOAASX 


SECTION A-A 


L R3 TO BE SELECTED PER ATP 1000287 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES, FROM IK THRU 4K OHMS IN STEPS OF 20 OHMS TWO 
RESISTORS MAY BE USED TO GET NEEDED VALUE. PER PART NO. 1010694. 

2. IDENTIFY USING DRAWING NO., REVISION LETTER, SERIAL NO. AND 
MANUFACTURERS SYMBOL PER MIL-STD-130. 

3. ENCAPSULATE WITH EPOXY PER NDI002036, CURING CYCLE B. 

4. ASSEMBLY TO MEET ALL REQUIREMENTS OF PSI000287. 

5. SOLDERING OF TERMINALS TO BE IN ACCORDANCE WITH MIL-STD-440, ALL OTHER 
ELECTRICAL CONNECTIONS SOLDER PER MIL-S-6872, WITH SN60WRAP2 SOLDER PER 0Q-S-57I. 

6. SOLDER COVER ASSEMBLY TO CASE PER MIL-8-6872 
WITH SN50WRAP2 SOLDER PER QQ-S-571. 

7. WINDING RESISTANCE FOR ACCEPTANCE TESTING: 

TERMINALS 182 0.1 OHM MAX. 

8. FINISH! VINYL WASH PER MIL-C-15328 AND ZINC CHROMATE PRIMER 
PER MIL-P-8585A, PAINT BLACK SEMI-GLOSS ENAMEL TT-E-529 
CLASS B COLOR 27038 PER FED STD 595. 

9. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED 
BY MIL -D-70327. 

K). INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A .007 GRAY 
FIBER SHEET PER MIL-I-695A TYPE F WITH A MINIMUM DIELECTRIC 
STRENGTH OF 250 VOLTS PER MIL 

II. CENTER IDENTIFICATION PLATE OVER POTTING HOLE. 


A/R WIRE_ 

A/R GRAY FIBER SHEET _ 

SCHEMATIC DIAGRAM 

1 DIODE 

2 DIODE _ • 

2 CAPACITOR _ 

2 RESISTOR _ 

I RESISTOR _ 

I TRANSFORMER ASSEMBLY 

I WIRING ASSEMBLY __ 

I CASE ASSEMBLY 

I COVER ASSEMBLY _ 

I PLATE-IDENTIFICATION 


UNUM OTHCMMK VCCtnCO 


UST OF PARTS ANO MATERIALS 


IMU BLOWER 
CURRENT SENSOR 



IOOI627 
1010439-2 
1010497 
10067 ST-IO 
1010693-97 
1010694 
IOOI629 
IOOI628 
1001631 
IOOI632 
' 1001543 





































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This specification consists of pages i 
to iv and 1 to 12 inclusive. 





ND-1002019 Markings 


















8 

■H 

3 






i 4~ 







APOLLO G&N Specification 
PS-1000287-F 

Class A Release 
TDRR 01266 
15 May 1963 


PROCUREMENT SPECIFICATION 
FOR 

IMU BLOWER CURRENT SENSOR 


■a 

Revision 

Letter 

TDRR 

No. 

Pages 

Revised 

Approval 

MIT 

NASA 

■■ 

03)69 

| mm 

UK 



Ig 

03337 


Sr 

A 

26 Nov. 1903 

F 

04809 

Pages 2, 3* 4, 5, 

6 & 9- 

ut( 

| 


— 












This specification consists of pages i 
to iv and 1 to 12 inclusive. 


















APOLLO G & N Specification 

PS-1000287-D 

17 Sept. 1963 


IMU BLOWER CURRENT SENSOR 


The purpose of this document is to establish the manufacturing and 
test requirements for procurement of IMU Blower Current Sensors for 
use in the Apollo Guidance and Navigation Equipment. 



ii 



APPROVED BY 


TITLE 


DATE 





APOLLO G & N Specification 

PS-1000287-D 

17 Sept. 1963 


PROCUREMENT SPECIFICATION 
FOR 

IMU BLOWER CURRENT SENSOR 


TABLE OF CONTENTS 

SECTION TITLE PAGE 

1 Scope. 1 

2 Applicable Documents 1 

3 Requirements 2 

4 Quality Assurance Provisions 8 

5 Preparation for Delivery 11 

6 Notes 11 


iv 


APOLLO G & N Specification 

PS-1000287-E 

17 Sep t . 1968" 

26 Sept. 1963 


PROCUREMENT SPECIFICATION 
FOR 

IMU BLOWER CURRENT SENSOR 


1. SCOPE 

1- 1 PURPOSE. This specification establishes the requirements for the 
procurement of the IMU Blower Current Sensor hereafter called sensor. 

2. APPLICABLE DOCUMENTS 

2- 1 EFFECTIVE ISSUES. The following documents of the issue in effect 
on the date of invitations for bids form a part of this specification to the 
extent specified herein. 

SPECIFICATIONS 


Military 

MIL-P-116 Preservation, Methods of 

MIL-E-17555 Electronic and Electrical Equipment and 

Associated Repair Parts, Preparation 
for Delivery of 


Apollo G & N 
ND-1002023 

ND-1002059 

ND-1015404 


ND-1002019 


Procedure for Serialization of Components, 
Assemblies, etc., for Apollo Guidance 
and Navigation equipment. 

Qualification Specification, Magnetic 
Amplifiers 

General Specification, Configuration, 
Process and Quality Control Requirements 
for Suppliers of High Reliability Articles 
for Use in Spacecraft and Supporting 
Equipment 

Marking, General Specification for 


1 


APOLLO G & N Specification 
PS-1000287-F 

17 OipL 1009. - 

26 Nov. 1963 


STANDARDS 

Federal 

FED-STD-595 Colors 

Military 

MIL-STD-130 Identification Marking of U.S. 

Military Property 

MIL-STD-202 Test Methods for Electronic and 

Electrical Component Parts 


DRAWINGS 

Apollo G & N 

1000287 IMU Blower Current Sensor 

1001629 Transformer Assembly 

(Copies of specifications, standards, drawings, and publications required 
by suppliers in connection with specific procurement functions should be 
obtained from the purchaser or as directed by the contracting officer). 

2-2 CONFLICTING REQUIREMENTS. In the event of conflict between the 
requirements of this specification and other spe ifications and drawings 
cited herein, resolution must be obtained from the MIT Apollo Management 
Office via the purchaser. 


3. REQUIREMENTS 

The requirements of this specification are classified under two 
headings: 

General Requirements which are defined in paragraph 3-2 
and Performance and Product Characteristics which are 
defined in paragraph 3-3. 

3-1 DESCRIPTION. The unit shall be a circuit module designed to monitor 
the current to the IMU blowers by providing an output signal for telemetering 
and to drive an indicating instrument (meter). 


2 


APOLLO G & N Specification 

PS-1000287-F 

17 Sopfr 10 S3— 

26 Nov. 1963 

3-2 GENERAL REQUIREMENTS. 

3-2.1 Qualification TeBt. When specified by the purchaser, a represent¬ 
ative sample of the sensors shall be manufactured using the methods 
and procedures proposed for the production lot. These shall be submitted 
to the NASA Inspector for qualification test at an activity designated in the 
contract or by the purchaser. 

These qualification tests are conducted to determine whether or not 
the sensors are being produced in compliance with the requirements 
of the contract, specification, and drawings. Failure of the sensors to 
meet these requirements may result in disqualification of the supplier as 
determined by NASA or the purchaser. 

Further production of the item by the supplier prior to approval of 
the purchaser or the completion of the qualification tests shall be a * 
supplier's risk. Requalification will be required at the discretion of NASA 
or the purchaser in the event that: (a) the supplier has modified the item, 

(b) the supplier has instituted a change in the material used or in his 
processing, or (c) the specification requirements for the item have been 
amended or revised sufficiently to affect the character of the item. 

The qualification tests will be conducted in accordance with the 
procedures specified in section 4 of this specification. 

3-2. 2 Requalification Test. When specified by the purchaser, the supplier 
shall submit one or more sensors to be selected from each production 
lot by the purchaser for submission to a designated testing activity to 
determine compliance of the sample (s) with the requirements of the contract, 
specification, and drawings. 

3-2. 3 Materials and Construction. The materials used in fabricating the 
sensors shall be in strict accordance with the applicable drawings and 
specifications referenced herein. Substitute materials shall be selected 
of such quality as to ensure that the equipment will meet the requirements 
of this specification and shall be subject to prior approval of the purchaser. 

3-2.4 Weight, D imensions, Finish, and Marking. The weight, dimensions, 
finish, and marking of the sensor shall comply with the requirements 
specified herein or on the applicable drawings. 

3-2.4.1 Weight. Weight of the sensor shall not exceed ? ounces. 

3-2.4. 2 Finish Finish shall be as specified on the applicable drawing. 


APOLLO G & N Specification 
PS-1000287-F 


17 Be t* . 19 63- 
80 Gcp h t. 10 9 0 - 
28 ixov, 1983 


3-2. 4. 3 Marking. Marking Shall be in accordance with MIL-STD-130 
drtd Specification ND-1002019, and as specified on the applicable drawing. 

3-2 5 Serial Numbers. Each sensor identified by General Arrangement 
(or Assembly) Drawing shall be identified by a serial number assigned 
in accordance with Specification ND-1002023. 


3-2. 6 Workmanship. The fabrication and finish of the sensor, its 
assemblies, suba's"i£mblies, and parts shall be such as to produce a unit 
free from any defect that would affect proper functioning in service. 


3-2. 7 Warranty. A warranty shall provide for the supplier to remedy by 
correction or replacement any component or end item found to be defective 
in material or workmanship not later than six (6) months after acceptance. 
The allowability of the cost of any such correction or replacement shall 
be determined as provided in the clauses of the appropriate contract entitled 
’’Allowable Cost, Fixed Fee and Payment, " and "Inspection and Correction 
of Defects. ” 


3-2.8 Service Life. 

3-2.8.1 Operating Life. The sensor design is intended to meet perform¬ 
ance specifications foFat least 20,000 hours of operating, excluding the 
supplier's test time of the complete unit. 

3-2. 8. 2 Shelf Life. The sensor design is intended to have a shelf life 
of at least 5 years, without operating, at ambient room temperature after 
final acceptance at the supplier's plant. 

3-3 PERFORMANCE AND PRODUCT CHARACTERISTICS. The following 
requirements are stated to inform the supplier of specific characteristics 
and of the goals that were considered in the design. Inclusion of this 
information shall not be construed by the supplier as authorization to 
modify the design. 

If the design of any part is not completely specified by the contractual 
documents, the supplier may submit a uggested design document for 
approval which will support these requit ments. 


If, in the opinion of the supplier, a; y design or testing shall impose 
undue time delay or expense, he shall so state, in detail, m a counter¬ 
proposal, substantiating all contributing factors when submitting a bid, 
proposal, or change request in connection with this specification. 


Requests for changes to or deviations from this specification or 
applicable drawings, specifications, publications, materials, or processes 
specified herein shall be accompanied by written justification. 


4 


APOLLO G & N Specification 
PS-10002L7- F 
17 Cep t . 1033 
flO Be pi. 100 9 - 
26 Nov. IS 6 3 

3-3.1 Functional Requirements. 

3-3.1.1 Winding Resistances. DC resistance of the windings shall be as 
specified in Apollo G & N Drawings 1000287 and 1001629. . . 

3-3.1. 2 Dielectric Strength. The sensor shall exhibit no evidence of 
breakdown when subjected to a 500V rms voltage. • • 

3-3.1. 3 Insulation Resistance. The insulation resistance of tne sensor 
shall be 100 megohms minimum. . . 

3-3.1.4 Performance. Performance of the sensor, when connected as 
shown in Figure 1, shall be as follows: 

3-3 1. 4.1 Gain. When operating into a 250K ±3 percent resistive load 
and when aTTto 1.0 ampere, 800 cps current is flowing through the input 
terminals, the unit shall provide an output of 0 to 5 vdc which is linearly 
proportional to the input. The maximum output voltage error siuill not 
exceed *4 percent of full scale over 10 to 100 percent of the output range. 
The unit shall operate as specified after reaching thermal stability with 
the ambient temperature specified in 4. 2.1 and again after reaching thermal 
stability with an ambient temperature of 150° * 5°F. When the ambient 
temperature is returned to that specified in 4. 2.1 and after thermal 
stabilization occurs, the unit shall again operate as specified. 


3-3.1.4. 2 Maximum Output. The output shall be internally limited to 
6. 0 vdc maximum. " ... 

3-3.1. 4. 3 Output Impedance. The output impedance of the unit shall 
not exceed 4, 000 ohms. • 

3-3.1.4. 4 Output Ripple. Output peak-to-peak ripple shall not exceed 
50 mv, ... 


5 


APOLLO G Si N Specification 
PS-1000287- F 
17 Gcpt. 10 S3 - - 
BC Oaptj 108ft - 
2b Nov. 19 0 3 


29V 

900 cps 



HI 

R2 

H3 

R4 

mi 

yo 


p.cfjn potentiometer 

1" - .'f, *;<, 

- - i . " ' 


*k # 

r 

o.i o V 


ac mill 1 ammeter, 
voltmeter, O.lvf 


0. r ^ accuracy 

ac curacy ( 1 megohm minimum input 


impedance) 


^lffure 1 


'est Setup 


APOLLO G & N Specification 

PS-1000287-D 

17 Sept. 1963 


3-3. 2 Environmental Requirements. The sensor shall be capable of 
meeting the requirements of Specification ND-1002059. When a particular 
requirement of Specification ND-1002059 includes the sensor's capability 
of operation while being subjected to an environment, this shall be construed 
to mean that an output of 2. 5 * 0. 2 vdc shall be maintained under standard 
operating conditions as defined in 6-1.1. 

3-3.3 Design Requirements. 

3-3. 3.1 Interchangeability. Unless otherwise specified, the sensor and 
its component parts shall \>e physically and functionally interchangeable 
without selection or fitting. 

3-3. 3. 2 Reliability. The sensor shall be capable of operating a minimum 
of 20,000 consecutive hours without maintenance under any combination of 
conditions specified herein and shall have a maximum failure rate of 0. 5 
failures per 1, 000,000 hours. 

3-3. 3 . 3. Radio Interference Suppression. The suppression of radio noise 
and interference shall be considered in the design of the sensor. 

3-3. 3. 4 Flammable Materials. Materials which may be ignited or cause 
an explosion shall not be used for construction applications where sparking 
or arcing could cause ignition. Materials which may inadvertently support 
combustion shall not be used. Flammable impregnating, potting or embedding 
compounds, when enclosed in fire-resistance containers, shall be acceptable. 

3 - 3 . 3 . 5 Toxic Materials. Materials which produce harmful toxic effects 
during service usage shall not be used. Where a suitable nontoxic material 
is not available, preventive measures shall be provided, subject to the 
approval of NASA. Materials which when ignited, produce toxic substances 
or vapors shall be avoided whenever practicable. 

3-3. 3. 6 Unstable Materials. Materials which are unstable or become 
unstable to the extent that they emit or deposit corrosive substances capable 
of causing corrosion or producing electrical leakage paths within an assembly 
under possible operating and storage conditions shall not be used during 
manufacture or recommended for use during maintenance. 

3-3. 3. 7 Corrosion, Moisture, and Fungus-Resistant Materials . Materials 
shall be selected for noncorrosive and nonhygroscopic characteristics and 
ability to resist the effects of corrosion, moisture and fungus. Preference 
shall be given to materials with inherent fungus resistance rather than 
reliance upon the application of surface fungistatic or fungicidal treatments. 

3-3. 3. 8 Dissimilar Metals . The use of dissimilar metals shall be avoided 
whenever practicable. Magnesium shall not be used except with prior 
approval of the purchaser or when so called for on the applicable Apollo 
G & N drawings. 


7 


APOLLO G & N Specification 

PS-1000287-D 

17 Sept. 1963 


4. QUALITY ASSURANCE PROVISIONS 

4-1 GENERAL. Unless otherwise specified herein, the supplier is respon¬ 
sible for the performance of all inspection requirements prior to submission 
for NASA inspection and acceptance. Except as otherwise specified, the 
supplier may utilize his own facilities or any commercial laboratory accept¬ 
able to NASA. InsDection records of the examinations and tests shall be 
kept complete and available to NASA as specified in the contract or order. 

The supplier shall conform to Class 1 of Specification ND 1015404. 

4-1.1 Acceptance Tests. These tests shall be accomplished on each 
sensor being submitted for acceptance under the contract. Acceptance 
test data on each unit accepted must accompany shipment to the purchaser. 
Acceptance tests shall be witnessed by the cognizant government inspector, 
a representative of the purchaser, or as the purchaser may direct in the 
procurement order. These tests are detailed in paragraph 4-2. Failure 
of the sensor to comply with these requirements shall result in rejection 
of the item or lot of items. 

4-1. 2 Qualification and Requalification Tests. Qualification and requali- 
fication tests shall be accomplished at a NASA designated activity. These 
tests, as outlined in paragraph 4-3, shall be conducted after the award of 
the contract to determine that the production will meet all requirements of 
this specification. Acceptance shall be based on no defects in the sensor. 

Failure of the sensor to comply with these requirements shall 
result in the rejection of the lot or the cessation of production, as determined 
by the procuring activity. 

4-2 ACCEPTANCE TESTS. 

4-2.1 Test Conditions. Unless otherwise specified herein, the sensor 
shall be subjected to tests under the following ambient conditions: 

Temperature 25 - 10°C 

Relative Humidity Not more than 90% 

Barometric Pressure 28 to 31 in. Hg 

4-2. 2 Test Power. The following electrical inpr f , as measured at the 
input of the unit under test, are necessary for teoting this item: 

28V rms -5 percent, 800 cps *5 percent. 


8 


APOLLO G & N Specification 
PS-1000287-F 

26 Nov. 1963 

4-2. 3 Visual and Mechanical Inspection. A comprehensive inspection shall 
be made*of the sensor to determine the extent of compliance with the require¬ 
ments of this specification and the applicable Apollo G &. N drawing specified 
in Section 2 and shall at least include determination of the following: 

a) Size, dimension, tolerance, weight, appearance and markings. 

b) Adequacy of materials, parts, and subassemblies; compliance 
with specific ratings, and conformance to applicable specifications. 

c) Finish, coatings, construction, markings, and nameplates, as 
applicable.. 

d) Wiring, cabling, welding, soldering, color coding, and terminals, 
as applicable. 

e) Workmanship and cleanup. 

4-2.4 Winding Resistances . DC resistance of the windings shall be tested 
using method 303 of MIL-STD-202 and shall be as specified on Apollo G & N 
drawings 1000287 and 1001629. * 

4-2. 5 Dielectric Strength. Dielectric strength shall be checked by applying 
a 500V rms, 60 cps~voItage between each terminal and the case and a 200V rms, 
60 cps (100 K source impedance) voltage between terminals 1 and 4. The leak¬ 
age current shall not exceed 1. 0 ma. This test shall be conducted in accordance 
with method 301 of MIL-STD-202. 

4-2.6 Insulation Resistance. Insulation resistance shall be checked by 
applying a 300 vdc^voltage (current limited to 6 uamp) between each terminal 
and the case and between terminals 1 and 4. The minimum acceptable resis - 
tance shall be 100 megohms. This test shall be conducted in accordance with 
method 302 of MIL-STD-202. 

4-2. 7 Performance. Performance of the sensor shall be checked as ^ 
follows': The test setup for these tests shall be as specified in Figure 1. 

Unless otherwise specified, switch SI shall be in the open position, and 
S2 shall be in the closed position. 


9 


APOLLO G & N Specification 

PS-1000287-D 

17 Sept. 1963 


4-2. 7.1 Gain. Adjust potentiometer R1 for the input currents specified 
in Table IT ^he corresponding output voltages shall be as specified 
in that taole "'his test shall be performed three times, once in each 
of the following ambient temperatures, in the sequence indicated, after 
the unit attains thermal stability in the ambient temperature: 

(a) The temperature specified in 4. 2.1. 

(b) 150°*5°F. 

(c) The temperature specified in 4. 2.1. 


Table I. Gain 


Input Current-Amperes 
(As indicated on meter Ml) 

Output Voltage - vdc 
(As indicated on meter M2) 

0. 0 (S2 open) 

0.0 ±0.0 

0 1 

0.5 ±0.2 

0.2 

0.4 

1.0 ±0.2 

2.0 ±0.2 

0.6 

3.0 ±0.2 

0.8 

4.0 *0.2 

1.0 

5.0 ±0.2 


4-2. 7. 2 Maximum Output. Adjust R1 for an indication of 1. 5 amperes 
on ML The voltage indicated on M2 shall not exceed 6. 0 vdc. 

4-2. 7. 3 Output Imped ance. Adjust R1 for an indication of 1.0 ampere 
on Ml and note the output voltage (M2). Close switch SI. The output voltage 
shall not decrease by more than 50 percent after SI is closed. 

4-2. 7. 4 Output Ripple. Connect a calibrated oscilloscope in parallel 
with M2. Adjust R1 for the input currents specified in Table I and for 
an input current of 1. 5 amperes. The peak-to-peak ripple shall not exceed 
50 mv for any of these input currents. 

4-3 QUALIFICATION AND REQUALIFICATION TESTS. Qualification and 
requalification tests shall be performed in accordance with Specification 
ND-1002059. When sensor operation is included as a condition in a test 
i- Specification ND-1002059, the sensor shall be operated under standard 
operating conditions (see6.1.1). The output shall be monitored and shall 
be 2. 5 *0. 2 vdc at all times. 


10 





APOLLO G & N Specification 

PS-1000287-D 

17 Sept. 1963 


5. PREPARATION FOR DELIVERY 

5-1 PRESERVATION AND PACKAGING. The sensor shall be preserved 
and packaged in accordance with Specification MIL-E-17555; level B, as 
specified in the contract or purchase order. 

5-1.1 Le vel B (Limited Military Packaging). Level B packaging is that 
which will afford adequate protection against damage during multiple 
domestic shipments, handling, and covered storage. 

5-1.1.1 Cleaning. Cleaning for Level B preservation and packaging shall 
be in accordance with method C -1 of Specification MIL-B-116. 

5-1.1. 2 Unit Protection. The sensor shall be individually afforded unit 
protection in accordance with method III of Specification MIL-P-116. In 
addition, equipment packaged for level B protection shall be sealed against 
water and dust by means of suitable wrapping. 

5-2 REPAIR PARTS. Repair parts shall have preservation and packaging 
per the applicable repair parts list and its packaging supplement. 

5-3 PACKING. The equipment shall be packed in accordance with Speci¬ 
fication MIL-E-17555, level B. 

5- 4 MARKING. In addition to any special marking required by the 
contract or order, the marking of unit, interior packages, and exterior 
shipping containers shall be in accordance with level B of Specification 
MIL-E-17555. 

6. NOTES 

6- 1 DEFINITIONS 

5-1.1 St andard Operating Condition s. For the purposes specified in 3-3. 2 
and 4-3, standard operating conditions shall be defined as operation of 
the sensor with the inputs and test connections specified in Figure 1 with 
the input adjusted to 0. 5 ampere, SI in the open position and S2 in the 
closed position. 


11 


APOLLO G & N Specification 

PS-1000287-D 

17 Sept. 1963 


Notice- When NASA drawings, specifications, or other data 
are used for any purpose other than in connection 
with a definitely related NASA procurement operation, 
NASA thereby incurs no responsibility nor any 
obligation whatsoever; and the fact that NASA may 
have formulated, furnished, or in any way supplied 
the said drawings, specifications, or other data 
is not to be regarded by implication or otherwise 
as in any manner licensing the holder or any other 
person or corporation, or conveying any rights or 
permission to manufacture, use, or sell any patented 
invention that may in any way be related thereto. 


12 





Z. 8 3 0 0 01 


REVISIONS 

DESCRIPTION 


* 


<&-* 
© — 

(D—> + 
©—»- 


INPUT 

CURRENT 


OUTPUT 

SIGNAL 


,375 


U9 1,09 
m9 ? s MAY 


.25 

2. oof 


•. 032DIA. WELDABLE 
4-REQ’O - 


• 4-~40NC-8A 
ORES MT& STUD 
2 peq'Q 


FOR INFORMATION ONLY 


POP DETAIL.ED SPECIFICATIONS SEE 
' POPCN a SC SPECIFICATION 1000887 
Ptocoee*t 6 t/r 


CLASS B RELEASE TDR No.< 


DATE 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


_ LIST OF PARTS AND MATERIALS 

inotrum^tation LAG IMU BLOWER CURRENT 


SENSOR 

(MAB5A-0 


PWAWM | UWR 
APMtovco ro«yMSC 

MIT/IL APPROVAL 


CODE IDENT. 


INSTRUMENTATION 
LABORATORY 
Gawwipok. Mam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1000287 


APPLICATION 




























* ; 

■it 


Apollo C|N Specification 
PS-1000287 
15 May 1963 
Class B Release 
TDRR OlXbt* 


PROCUREMENT SPECIFICATION 
FOR 

IMU BLOWER CURRENT SENSOR (MA2SA-1) 


Record of Revisions 


Rcwision 

Latter 

TDRR 

No, 

Pages 

Approvals 

DATE 

Revised 

MIT NASA 






















TMjs specification consists of Page i to iii and 
1 tio 9 inclusive* 


Apollo G | N Specification 

PS-1000287 

15 May 1963 


*?_ % 

IMU PiAeR CURRENT SENSOR (MA25A-1) 

^ " 


. / 

' • 


i 


The purpose of this document is to establish the manufacturing and 
test requirements for procurement. The IMJ Blower Current Sensor 
(MA25A-1) is intended for use in the Apollo Guidance and Navigation 
Equipment program. 



Apollo G 6 N Specification 

PS-1000287 

15 May 1963 


PROCUREWNT SPECIFICATION 



IMU BLOWER CURRENT SENSOR (MA 2SA-1) 

1. 

SCOPE 


1.1 

SCOPE, This specification establishes the requirements for the pro¬ 
curement of the IMU Blower Current Sensor (MA25A-1) hereinafter 
called sensor. 

2. 

APPLICABLE DOCUMENTS 


2.1 

The following documents of the issue in effect on the date of invitation 
for bids form a part of this specification to the extent specified 
herein. 


SPECIFICATIONS 



Military 



MIL-T-27 

Transformers and Inductors (Audio, Power, 
and Pulse) 


MIL-P-116 

Preservation, Methods of 


MIL-I-16910 

Interference Measurement, Radio, Methods 
and Limits, 14 Kilocycles to 1000 Megacycles 


MIL-E-17555 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of 


Apollo G|N 



< ND-1002023 

Procedure for Serialization of Components, 
Assemblies, etc,, for Apollo Guidance and 
Navigation Equipment 


ND-1015404 

General Specification, Configuration, Pro¬ 
cess and Ouality Control Requirements for 
Suppliers of High Reliability Articles for 

Use in Spacecraft and Supporting Equipment. 


i 


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notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH Ml L"D"70327 

2 . IDENTIFY USING DRAWING NO., REVISION LETTER, 

SERIAL NO. ANO MANUFACTURERS SYMBOL 

PER MIL"STD"130 
3- WINDINGS 

GATE WINDINGS , EACH 
400 TURNS AWG 31 
TERMINALS 7 8 8 

CONTROL WINDINGS, EACH 
36 TURNS AWG 23 
TERMINALS 18 4,283 

BIAS WINDING 
1000 TURNS AWG 39 
TERMINALS 58 6 

4. RESISTORS TO BE SELECTED AT ASSEMBLY 

RANGE OF VALUES, FROM 600 OHMS THRU 800 OHMS EACH 
IN STEPS OF 10 OHMS 

5. ALUMINUM ALLOY 6061" T6 
PER SPEC QQ-A-327 TEMP T6 

6. ENCAPSULATE WITH EPOXY PER NDI002036. CURING CYCLE B 

7. CONTROL AND BIAS WINDINGS SHALL BE COMMON 
WOUND TO BOTH CORES 

B. GLASS FIBER FILLED DlALLYL" PHTHALATE 
PER MIL M*I9833"GDI "30"F* 

9. ASSEMBLY TO MEET REQUIREMENTS OF PS 1000288 

10. BASE TO BE COVERED WITH INSULATING TAPE 
PER MIL-I'19166 

11. TEFLON WIRE TYPE E AWG 26 
PER MIL" W-I6878/4A 

12. USE SNIO SOLDER 
PER SPEC QQ-S-571 

13 BREAK SHARP EDGES .010 MAX 


. WINDING RESISTANCE FOR 
ACCEPTANCE TESTING! 

GATE WINDINGS 4.50HMS±5% EACH 
TERMINALS 78 8 

CONTROL WINDINGS 0.15 OHMS MAX EACH 
TERMINALS 18 4,283 

BIAS WINDING 130 OHMS ±5% 

' TERMINALS 986 

BIAS WINDING PADDING RESISTOR 350 0HMSl20% 
TERMINALS 5 8 10 



SECTION B-B 
SCALE 2/1 


_ __ DIA 
•065 

10 HOLES SPACED AS SHOWN 


.045 

.035“ 



REPLACES 
REV. A WITH 
CHANGES 


A/R 

WIRE 



SEE NOTE II 

10 


A/R 

WIRE 

1010603-031 


SEE <OTE 3 

9 


A/R 

WIRE 

1010603-023 


_ 

_ 

nr 


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WIRE 

1010603-039 


3 

._ 

7 


10 

TERMINAL 

1010601 



6 


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COVER 



SEE NOTE 8 

5 


2 

RESISTOR 

1010604 


SEE NOTE 4 

4 


2 

CORE 

1010602 



3 


A/R 

TAPE 



SEE NOT£iC 

.X 


1 

BASE 



SEE NOTE 5 



QTV 

RCQO 

NOMENCLATURE 

OR DC SCRIPTION 

PART OR 

KXNTIFY1NG NO. 

sPcancATioN 

MATERIAL 

OR NOTES 

F1NC 

NO. 



SECTION c-c 

SCALE 2/1 


r 




unless otherwise stccmco 



dimensions mk m inches 

TOLERANCES ON 

FRACTIONS DECIMALS win 







00 NOT SCALE TMi ORANRNO 

1000202 

DLI00G2CI 

MATERIAL; 

/ 

1 

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UKD ON 

1 AmiCATION 

J ---- 1— 


T 




LIST OF PARTS ANO MATERIALS 


MMTNUMENTATION CAS 


m 


_££L, 


^H3 

A—owyo. MSC f 

MIT/ILAPWIOVAL I MIC 




SATURABLE 
REACTOR 

IMU BLOWER SPEED 
CONTROL 


-UIT 

MfTNUM ENT ATtOM 
LABORATORY 


1000268 


SHEET | 


INCHES 


PHOTOORAPHIC SCALE ONLY 








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ND-1015404 General Specification, Configuration, Pro¬ 

cess and Quality Control Requirements for 
Suppliers of High Reliability Articles for 
Use In Spacecraft and Supporting Equipment. 










SEE NOTE 12 



B REPLACES REV A WITH 
CHANGES 6 UPGRADED 
CLASS m TDRR 

~ revised per, Toea__ 


SCALE 4/1 


EMERGENCY Q. 
HEATERS (Z 


CONTROL (2 
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A*"\ 





~ 28V 
7) 800 CPS 


SEE DETAIL 


r SECTION A-A 
SCALE 2/I 


OVDC BIAS 

RESISTOR 


SCHEMATIC 


L INTERPRET DRAWING IN ACCORDANCE WITH MIL'D-70327 

2. IDENTIFY USING DRAWING NO., REVISION LETTER, 

SERIAL NO. AND MANUFACTURERS SYMBOL 

! PER MIL* STD* 130 

3. WINDINGS 

GATE WINDINGS, EACH 
r 400 TURNS AWG 31 
TERMINALS 7 a 9 

CONTROL WINDINGS, EACH 
36 TURNS AWG 23 
TERMINALS 18 4,283 

BIAS WINDING 
1000 TURNS AWG 39 
TERMINALS 586 


5. ALUMINUM ALLOY 6061-T6 
PER SPEC QQ-A-327 TEMP T 6 

6 . ENCAPSULATE WITH EPOXY PER HD 1002036. CURING CYCLE B 

7. CONTROL AND BIAS WINDINGS SHALL BE COMMON 
WOUND TO BOTH CORES 

•.GLASS EPOXY TUBING TYPE GEE 
PER MIL*P " I8I77B 

•.ASSEMBLY TO MEET REQUIREMENTS OF PS 1000288 
10.BASE TO BE COVERED WITH INSULATING TAPE 
PER MIL* I-19166 


14. WINDING RESISTANCE FOR 
ACCEPTANCE TESTING*. 

GATE WINDINGS 4.4OHMS ± 15% EACH 
TERMINALS 78 8 

CONTROL WINDINGS 0.15 OHMS MAX EACH 
TERMINALS 18 4,283 

BIAS WINDING 125 OHMS ±15% 

• TERMINALS 5 8 6 


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if ro 



15* 12* 

4 PLACES 



22.5*12* 
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SECTION B-B 
SCALE 2/1 


.065 

8 HOLES SPACED AS SHOWN 


12. USE SNIO SOLDER ^ 

PER SPEC QQ-8-871 

13 BREAK SHARP EDGES .010 MAX 


•045_ II 

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1010603-031 
~ 1010603-023 ~ 
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1010601 

" 1010629 
1010602 


SEE N0TE8 3 

4 

[SEE NOltc ~ 2 ~ 
SEE NOTES I 


1.60 

SECTION C-C 
t SCALE 2/1 


LIST Of PARTS ANO MATERIALS 

4* SATURABLE 
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IMU BLOWER SPEED 
CONTROL 


fmCECRARCCNTER 

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SCALE 4/1 


EMERGENCY Cl 
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_ REVISIONS _ 

DESCRIPTION ~DP»- 

' REPLACES REV A WITH $- Z w 

CHANGES 8 UPGRADED 
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REVISED PER. TD2R. Q f l/\^ 

' %CV15£DP£Z TOtZ putf 7/^/w5 



~ 28V 

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SEE DETAIL 


SECTION A-A 
SCALE 2/1 


OVDC BIAS 

RESISTOR 


SCHEMATIC 


notes: 

L INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 
2. IDENTIFY USING DRAWING NO., REVISION LETTER, 

SERIAL NO. AND MANUFACTURERS SYMBOL 
PER MIL-STD*130 
5. WINDINGS 

GATE WINDINGS, EACH 
400 TURNS AWG 31 
TERMINALS 7 8 8 

CONTROL WINDINGS, EACH 
36 TURNS AWG 23 
TERMINALS 18 4,283 

BIAS WINDING 
1000 TURNS AWG 39 
TERMINALS 586 


5. ALUMINUM ALLOY 6061-T6 
PER SPEC QQ-A-327 TEMP T6 

6 . ENCAPSULATE WITH EPOXY PER ND1002036. CURING CYCLE B 

7. CONTROL AND BIAS WINDINGS SHALL BE COMMON 
WOUND TO BOTH CORES 

B. GLASS EPOXY TUBING TYPE GEE 
PER MIL" P ‘ I8I77B 

a ASSEMBLY TO MEET REQUIREMENTS OF PS 1000288 
10.BASE TO BE COVERED WITH INSULATING TAPE 
PER MIL'1-19166 



14. WINDING RESISTANCE FOR 
ACCEPTANCE TESTING*. 

GATE WINDINGS 4.4OHMS ± 15% EACH 
TERMINALS 78 8 

CONTROL WINDINGS 0.15 OHMS MAX EACH 
TERMINALS 184,283 

BIAS WINDING 125 OHMS 115% 

* TERMINALS 58 6 


20 ° ± 2 ° 

4 PLACES 



- 30® 12® 
4 PLACES 



SECTION B-B 
SCALE 2/1 


.065 

8 HOLES SPACED AS SHOWN 


12. USE SNIO SOLDER 
PER SPEC QQ-S-571 

13 BREAK SHARP EDGES .010 MAX 



-!*5£dia 

1.05 


.130 

2 HOLES 


REPLACES 
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COVER _ 

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TAPE _ 

BASE_ 


1010603-031 
" 1010603-023 ' 
~ 1010603-039 ' 
1010601 

1010629*" 

1010602 


SEE NOTE IC 
"SEE NOTES 


UNLESS OTHERWISE SPECIFIED 


'*4- 


LIST OF PARTS AMO MATERIALS 

■» SATURABLE 
REACTOR 

IMU BLOWER SPEED 
CONTROL 


SECTION 
I SCALE 2/1 


SPACECRAFT CENTER 
HOUSTON TEXAS 
NMA OT U WIN fi NO. 

10002 88 


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SEE NOTE 12 



I EMERGENCY Q. 
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CONTROL 
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•820 MAX 

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SEE DETAIL 



B REPLACES REV A WITH 

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~ REVISED PEE TOER ^ 

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r SECTION A'A 
SCALE 2/1 


OVDC BIAS 

RESISTOR 


SCHEMATIC 


.775 B 

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.765 a 

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L INTERPRET DRAWING IN ACCORDANCE WITH MIL'D’70327 
z. IDENTIFY USING DRAWING NO., REVISION LETTER, 

SERIAL NO. AND MANUFACTURERS SYMBOL 
i PER MIL" STD* 150 . 

& WINDINGS 

GATE WINDINGS, EACH ^ 

* ■ 400 TURNS AV.G 31 , , 

* TERMINALS 7S8 , 

CONTROL WINDINGS, EACH 
36 TURNS AWG 23 
TERMINALS 164,233 

BIAS WINDING 
1000 TURNS AWG 39 
TERMINALS 58 6 


14. WINDING RESISTANCE FOR 
ACCEPTANCE TESTING*. 

GATE WINDINGS 4.4OHMS ± 15% EACH 
TERMINALS 78 8 

CONTROL WINDINGS 0.15 OHMS MAX EACH 
TERMINALS 18 4,2 83 

BIAS WINDING 125 OHMS ±15% 

* TERMINALS 58 6 


20* ±2* 

4 PLACES 



- 30* 12* 
4 PLACES 


SECTION B-B 
SCALE 2/1 


.065 

8 HOLES SPACED AS SHOWN 




5. ALUMINUM ALLOY 6061"T« 

PER SPEC QQ-A-327 TEMP T6 

6 . ENCAPSULATE WITH EPOXY PER NDI002036. CURING CYCLE B 
T. CONTROL AND BIAS WINDINGS SHALL BE COMMON 

WOUND TO BOTH CORES 

9. GLASS EPOXY TUBING TYPE GEE ^ ' 

PER MIL-P-I8I77B 

■%ASSEMBLY TO MEET REQUIREMENTS OF PS 1000288 

10. BASE TO BE COVERED WITH INSULATING TAPE 
PER MIL’ 1"19166 


tf.USE SNIO SOLDER 
PER SPEC QQ-S-571 

13 BREAK SHARP EDGES X) 10 MAX 


£ .045 II 

* ' ••040 — ItT 



036 R REPLACES 

026 4 PLACES REV. A WITH 

o*. CHANGES 


SECTION C C 


WIRE _ 

WIRE 

WIRE _ 

TERMINAL 

COVER _ 

SELF-CLINCHING STUD 
CORE_ 


1006711-14 
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‘ 1 -21 
1010601*1 

1010629-f 
1010602 


_6_ 

:N0TE8 5 


SEE NOTE C 
“ SEE n6te S 


UNLESS OTH CT WtS C SKCmCO 


LIST OF PARTS AND MATERIALS 

A. SATURABLE 
REACTOR 

IMU BLOWER SPEED 
CONTROL . 


1000288 





















































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SEE NOTE 12 



B REPLACES REV A WITH 
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EMERGENCY (i 
HEATERS (Z 


CONTROL (2 
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A*\ 


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SECTION A-A 
SCALE 2/1 


OVDC BIAS 

RESISTOR 


SCHEMATIC 


notes: 

I* INTERPRET DRAWING IN ACCORDANCE WITH MIL‘D-70327 

2. IDENTIFY USING DRAWING NO., REVISION LETTER, 

SERIAL NO. AND MANUFACTURERS SYMBOL 

1 PER MIL-STD*130 

3. WINDINGS 

GATE WINOINGS, EACH 
400 TURNS AWG 31 
TERMINALS 7 8 8 

CONTROL WINDINGS, EACH 
36 TURNS AWG 23 
TERMINALS 18 4,283 

BIAS WINDING 
1000 TURNS AWG 39 
TERMINALS 58 6 


5. ALUMINUM ALLOY 6061-T6 
PER SPEC QQ-A-327 TEMP T6 

6 . ENCAPSULATE WITH EPOXY PER ND1002036. CURING CYCLE B 

7. CONTROL AND 81 AS WINDINGS SHALL BE COMMON 
WOUND TO BOTH CORES 

8 . GLASS EPOXY TUBING TYPE GEE 

PER MIL-P-I8I77B . . 

9. ASSEMBLY TO MEET REQUIREMENTS OF PS 1000288 

10. BASE TO BE COVERED WITH INSULATING TAPE 
PER MIL- I- 19166 



14. WINDING RESISTANCE FOR 
ACCEPTANCE TESTING*. 

GATE WINDINGS 4.4OHMS ± 15% EACH 

(2.2 OHMS ±15% PARALLEL WINDING RESISTANCE) 

TERMINALS 7 8 8 

CONTROL WINDINGS 0.15 OHMS MAX EACH 
TERMINALS 18 4,283 

BIAS WINDING 125 OHMS ±15% 

TERMINALS 5 8 6 


20 ° 12 ° 

4 PLACES 



- 30* 12® 
4 PLACES 


SECTION B-B 
SCALE 2/1 


.065 

8 HOLES SPACED AS SHOWN 


g 

fil 

III 


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1.05 U 


e. USE SNIO SOLDER 
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036 _ REPLACES 

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1010629-1~ 
1010602 


SEE NOTE IC 
"SEE NOTES 


UNLESS OTMERWISC SKOFICO 


00 NOT SCAU TINS ONAWINS 


1.60 

SECTION OC 
| SCALE 2 /I 


LIST OF PARTS AND MATERIALS 

if SATURABLE 
REACTOR 

IMU BLOWER SPEED 
CONTROL 


1000288 



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SEE NOTE 12 


SWAGED 



DETAIL A 
SCALE 4/1 


12 3 4 


■ A^\ 




I EMERGENCY ©■ 
HEATERS 0_ 


CONTROL (1 
HEATERS ^ 



SEE NOTE 18 


i 


Q. 


<3\ 

9 


ZONE 

SYM 

DCSCmrnON 



* 

B 

REPLACES REV A WITH 
CHANGES 8 UPGRADED " 
CLASS A TDRR 0/399 




C 

REVISED PEE TOER. 




D 

%CV15£D P£* TO**. 

WO* 



— 

*£\/t5U> AC* 7T>*4 03734- 




F 

*£tf/S£D P£* 710*3 0*99 + 

>-5*3 

vV. 


~ 

ALA FOAA 05**9 

3 

UL I 


w 28V 
<y 800 CPS 

4—(5) BLOWER 


SEE DETAIL 


OVDC BIAS 

RESISTOR 


SCHEMATIC 


notes: 

fw INTERPRET DRAWING IN ACCORDANCE WITH MIL‘D-70327 
, Z, IDENTIFY USING DRAWING NO., REVISION LETTER, 

> SERIAL NO. AND MANUFACTURERS SYMBOL 
i i PER MIL-STD*130 

8 . WINDINGS 

GATE WINDINGS, EACH 
400 TURNS AWG 31 . • „ 

« ' TERMINALS 78 8 

CONTROL WINDINGS, EACH 
36 TURNS AWG 23 
TERMINALS 184,283 

BIAS WINDING 
1000 TURNS AWG 39 
TERMINALS 586 

4. PREHEAT WINDING AND IMPREGNANT TO 250°F 
IMPREGNATE WINDING WITH IMPREGNANT. 

PULL VACUUM OF 10" H« obs 

s BAKE 24 HOURS AT 180° F. 

5. ALUMINUM ALLOY 6061-T6 
PER SPEC QQ-A-327 TEMP T6 

8 . ENCAPSULATE WITH EPOXY PER NDI002036. CURING CYCLE B 

7. CONTROL AND BIAS WINDINGS SHALL BE COMMON 
WOUND TO BOTH CORES 

8 . GLASS EPOXY TUBING TYPE GEE 
PER MIL'P* I8I77B 

8 .ASSEMBLY TO MEET REQUIREMENTS OF PS 1000288 

10. BASE TO BE COVERED WITH INSULATING TAPE 
PER MIL- I-19166 

11. WIPE IMPREGNATION DURING CURE CYCLE 

/ V 18 .SOLDERING OF ELECTRICAL CONNECTIONS TO BE 
IN ACCORDANCE WITH MIL-$TP-440 
WITH SNI0WARP2 SOLDER PER QQ-S-571 

is break sharp edges jo \omax 





"* 1.05 D,A * 

i 

B 



.740 ▲ 

I L 

+ - 0 - 9-1 - 

_L 


14. winding resistance for 

ACCEPTANCE TESTING*. 

GATE WINDINGS 4.4 OHMS ± 15% EACH 

(2.2 OHMS ±15% PARALLEL WINDING RESISTANCE) 

TERMINALS 7 8 8 

CONTROL WINDINGS 0.15 OHMS MAX EACH 
TERMINALS 18 4,283 

. BIAS WINDING 125 OHMS ±15% 

TERMINALS 5 8 6 

15.1/32“ GLASS EPOXY SHEET TYPE GEE 
PER MIL-P-I8I77B 

16. ADJUST RESISTANCE OF BIAS WINDING BY 
WRAPPING EXTRA LEAD OF BIAS WINDING 
AROUND THE PERIPHERY OF THE WOUND REACTOR 

17. BEFORE WINDING, TEMPERATURE CYCLE CORES 
FOR A MINIMUM OF 5 DAYS PER NDI002209, 

CORE MUST MEET REQUIREMENTS OF SCO 1010602 
AFTER TEMPERATURE CYCLING 

18. (9) DENOTES THE SAME INSTANTANEOUS 

POLARITY 

19. FINISH*. VINYL WASH PER MIL-C-15328, 

PAINT BLACK SEMI-GLOSS 
i ! ENAMEL TT-E-529 CLASS B, 

COLOR 27038 PER FED. STD 595 

20. MARK TERMINAL NUMBERS ABOVE TERMINALS 
AS SHOWN, AND IDENTIFYING INFORMATION 

I PER NOTE 2 ON TOP OF REACTOR, 
i PER NDI0020I9 AND ND1002122 
TYPE IT CLASS X 


















































SEE NOTE 12 



EMERGENCY Cl 
HEATERS (2 


SCALE 4/1 


CONTROL C£ 
HEATERS 


,820 MAX 
AFTER 
POTTING 





SEE NOTE 18 


B REPLACES RFV A WITH 
CHANGES 8 UPGRADED * 
CLASS A TDRH 0 , 3 ? + 


~ 28V 
z) 800 CPS 


C REVISED PER TDeR 0 f IfS** IT 

~ tcvtsep P£* rot* outf~ l/*4* lilL 
T~~ qcvtsu * c* rot* rffX. 

F «£WS£D PS4 n>4* o 299 + y*'*3 V//> 
~G~~ /j£V/S£0 r&*A 05'*9 '*’*+) ill 
' H \flEVf50F FEfi TPM 116*0 


SEE DETAIL 


SECTION A-A 
SCALE 2/1 


(a) ® 

OVDC BIAS 

RESISTOR 


SCHEMATIC 



, INTERPRET DRAWING IN ACCORDANCE WITH MIL”D”70327 
.IDENTIFY USING DRAWING NO-, REVISION LETTER, 

SERIAL NO. AND MANUFACTURERS SYMBOL 

PER MIL”STD"130 

WINDINGS 

GATE WINDINGS , EACH 
400 TURNS AWG 31 
TERMINALS 7 a 8 


. WINDING RESISTANCE FOR 
ACCEPTANCE TESTING*. 

GATE WINDINGS 4.4OHMS 115% EACH 

(2.2 OHMS 115% PARALLEL WINDING RESISTANCE) 

TERMINALS 7 ft 8 


- 20 ° ± 2 ° 

4 PLACES 


- 30® 12® 
4 PLACES 


CONTROL WINDINGS 0.15 OHMS MAX EACH 
TERMINALS I a 4, 28 3 


CONTROL WINDINGS, EACH 
36 TURNS AWG 23 
TERMINALS 18 4,283 


BIAS WINDING 
1000 TURNS AWG 39 
TERMINALS 5 8 6 

.PREHEAT WINDING AND IMPREGNANT TO 250°F 
IMPREGNATE WINDING WITH IMPREGNANT. 

PULL VACUUM OF lO"Hfl obs 
BAKE 24 HOURS AT 180° F. 


BIAS WINDING 125 OHMS ±15% 

TERMINALS 5 ft 6 

15. 1/32** GLASS EPOXY SHEET TYPE GEE 
PER MIL-P”I8I77B 

16. ADJUST RESISTANCE OF BIAS WINDING BY 
WRAPPING EXTRA LEAD OF BIAS WINDING 
AROUND THE PERIPHERY OF THE WOUND REACTOR 

17. BEFORE WINDING, TEMPERATURE CYCLE CORES 
FOR A MINIMUM OF 5 DAYS PER NDI002209, 
CORE MUST MEET REQUIREMENTS OF SCD 1010602 
AFTER TEMPERATURE CYCLING 


SCALE 2/1 
DETAIL OF ITEM 10 


SECTION B'B^ 
SCALE 2/1 
DETAIL OF ITEM 5 


.065 

8 HOLES SP; ~ED AS SHOWN 


18.(■) DENOTES THE SAME INSTANTANEOUS 
POLARITY 


jA/R | IMPREGNANT 


11010687- l~ 


. DIA THRU - 



.ALUMINUM ALLOY 606 I” T6 . 
PER SPEC QU-A-327 TEMP T6 


^ENCAPSULATE WITH EPOXY PER ND1002036. CURING CYCLE B 
’.CONTROL AND BIAS WINDINGS SHALL BE COMMON 
WOUND TO BOTH CORES 


.GLASS EPOXY TUBING TYPE GEE 
PER MIL” P ” 18177B 


19. FINISH*. VINYL WASH PER MIL”C*I5328, 

PAINT BLACK SEMI'GLOSS 
ENAMEL TT-E-529 CLASS B, 

COLOR 27038 PER FED. STD 595 

20. MARK TERMINAL NUMBERS ABOVE TERMINALS 
AS SHOWN, AND IDENTIFYING INFORMATION 
PER NOTE 2 ON TOP OF REACTOR, 

PER ND 1002019 AND NDI002I22 
TYPE H CLASS Z 


REPLACES 


I. ASSEMBLY TO MEET REQUIREMENTS OF PS 1000288 
).BASE TO BE COVERED WITH INSULATING TAPE 


PER MIL* I-19166 


.WIPE IMPREGNATION DURING CURE CYCLE 
». SOLDER INC OF ELECTRICAL CONNECTIONS TO BE 
IN ACCORDANCE WITH MIL”STD-440 
WITH SN10WARP2 SOLDER PER QQ'S”57| 


u 

.045 II 
.040 I \ 



— ;o26 4PLACES REV. A WITH 

j3o dia - changes 

2 HOLES 


PLATE-TOP _ 

WIRE 

WIRE _ 

WIRE __ 

‘ TERMINAL _ 

COVER 

SELF-CLINCHING STUD 
CORE J 

r TAPE __ 

BASE _ 


" 1006711-14" 
- 12 ~ 
1 *2l' 

I0I060I-I 


£E NOTE 151 
5EEN0TE3 9 


SEE N0TE8T 


1010629”! 

1010602 


" SEE NOTE" 
"SEE NOTE^ 


NOMENCLATURE 
OR DESCRIPTION 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE M INCHES 
TOLERANCES ON 

FRACTIONS occmmu ans les 


LIST Of PARTS AND MATERIALS 

SATURABLE 

REACTOR 


IM9TNUM CNTATION 

laboratory 


13 BREAK SHARP EDGES .010 MAX 


1.64_ 

1.60 

SCALE 2 / I 
DETAIL OF ITEM I 


_ 1010039 °° "° 

1000202 DU0CC2CI 

NEAT ASST USED ON 

APPLICATION 

1 - r_ ^ 


DO NOT SCALE TINS DRAW! NO 


IMU BLOWER SPEED 
CONTROL 


SPACECRAFT CENTER 
HOUSTON TEXAS 



IGOG288 




Mil* 3E3K5?* TLJ l, *"RW'HLs 

























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notes: 


1. INTERPRET DRAWING IN ACCORDANCE WITH MIL*D*70327 

2. IDENTIFY USING DRAWING NO., REVISION LETTER, 

* SERIAL NO. AND MANUFACTURERS SYMBOL 

PER MIL-STD-130 

3. WINDINGS 

GATE windings , each 
400 URNS AWG SI 
TERMINALS 7 6 8 


CONTROL WINDINGS 
76 TURNS AW G 27 
TERMINALS I 5k 4 , 


, EACH 

2 a 3 


BIAS WINDING 

10 00 TURNS AWL 39 

TERMINALS b h 6 

4. PREHEAT WINDING AND IMPREGNANT TO 25C 


IMPREGNATE WINDING WITH IMPRLGNANT. 
PJuu VACUUM OF I0"HqObs 
BAKE >5 -Cl -S M N. at ;,()■- f-. 

LOY 606 T6 
w^-A-32" 7 TE'VP T 6 


* M i N 


0 . 


.C AP : 


.ate A ; ’ ‘ 


'.'i 


BIAS W m L 
, Th CORES 


S EPOXY TLB: NG TYPE GEE 
FEN MIL - P - 18! ’’78 

9. a-:pmFi.y Td me-T Rf .UiREMENTS OF PS 10 0 0288 
0. B 4 f rrs - bf C'U^P A i T H INSULATING TAPE 


11. WIPE IMPREGNATION DURING CURE CYCLE 

12. SOLDER'NG OF ELECTRICAL CONN “CHONS TO BE 
t N ;. C <u i \ D A NO l W . . 11 M > ' c • D * ' 4 _ 

WITH SNI0WARP2 SOLDER PER QA-S-57I 


.760 

.740 


14. WINDING RESISTANCE FOR 

ACCEPTANCE TESTING! AT 2o s U‘’C 

GATE WINDINGS 4.4 OHMS ± 15% E AC-H 

(2.2 OHMS 115% PARALLEL WINDING RESISTANCE) 

TERMINALS 7 6 8 


CONTROL WINDINGS 0-15 OHMS MAX EACH 
TERMINALS 16 4, 263 


I 36. CURING CYCLE 6 
COMMON 


BIAS WINDING 125 OHMS ±15% 

TERMINALS 5 6 6 

15. 1/32" GLASS EPOXY SHEET TYPE GEE 
PER MIL-P-181 77B 

16 ADJUST RESISTANCE OF BIAS WINDING BY 
WRAPPING EXTRA i_EAD OF BIAS WINDING 
AROUND THE PERIPHERY OF THE WOUND REACTOR 

17. BEFORE WINDING, TEMPERATURE CYCLt CORES 
FOR A MINIMUM Of 5 DAYS PER ND1002209, 
CORE Must MEET REQUIREMENTS OF SCO 1010602 
AFTER TEMPERATURE CYCLING 

18. (■) DENOTES THE SAME INSTANTANEOUS 

POLARITY 

19. FINISH; VINYL WASH PER MIL-C-i5328, 

PAINT BLACK SEMI GLOSS 
ENAMEL TT-E'529 CLASS B, 

COLOR 2 7 038 PER FED. STD 595 

20. MARK TERMINAL NUMBERS ABOVE TERMINALS 
A c SHOWN AND IDENTIFYING INFORMATION 
PER NOTE 2 ON TOP OF REACTOR, 

PER ND 100201 9 AND NDI002I22 
TYPE IT .CLASS T 

II. v* .* / H t\ '-N. - r F .*• L 1 CN: *> . A „ 5: T- = H, 

P - - 2 R i.. u c f. IR! L r 0 - j !/1 2 - so*.. 


:mU d,a 


w.r- 


.045 

.040 


!* bkfak Sharp edges .010 max 


3 


2 



; J2 6t 



















AdoIIo G & N Specification 
PS-1000288-* 

Class A Release 
TDRR 01206 
15 May 1963 


PROCUREMENT SPECIFICATION 
FOR 

SATURABLE REACTOR 
(APOLLO IMU BLOWER SPEED CONTROL) 


Record of Revisions 



TDRR 

Pages 

Revised 

AoDrovals 


Revision 

Letter 

No. 

MIT 

NASA 

DATE 

A 

01382 

'All pages rSvfSTfffl; 
was 13 pages, now 11 



3 

0 f 

B 


Pages 3,6 49 

idhL— 


C 


Pages i and 4 

Hi , 

JA. 

31 July 63' 

D 

02628 

Page 6 


/ 

21 Aug '63 

_5 . 

-. ".“ .*.1 

1 

32623.,,.._ 1 

Pages 2,4,7,8,9, 

i.M,- 


21 Aug '63 

V 

02993 

Page 6 

M£- 


c Sept *63 

G 

0480? 

Pages 3 and 10 



26 Nov.'63 

H 

04808 

P«.a I.3.4.8.9. 

apd 10 , 

U/li r . 


26 Hov.*63 

J 

.iIM 

Pages 5 and 10 

wF 

M— 

25 Aug '64 


This specification consists of Pages 1 
to lv and 1 to 11 Inclusive. 


I 


Apollo G & N Specification 

PS-1000P88-A 

29 May 1963 


SATURABLE REACTOR 
(APOLLO IMU BLOWER SPEED CONTROL) 


The purpose of this document is to establish the manufacturing 
and test requirements for procurement of the Saturable Reactor 
(Aoollo IMU Blower Speed Control) which Is intended for use in the 
Apollo Guidance and Navigation Equipment program. 



MIT INSTRUMENTATION LABORATORY ; 


NASA/MSC APPROVAL 


ii 



APPROVED BY 


TITLE 


DATE 


Apollo a & N Specification 
PS-1000?88-A 

29 May 1963 


PROCUREMENT SPECIFICATION 
FOR 

SATURABLE REACTOR 
(APOLLO IMU BLOWER SPEED CONTROL) 


TABLE OF CONTENTS 


SECTION 


PAGE 


1 

2 

3 

4 

5 

6 


SCOPE.- 

APPLICABLE DOCUMENTS .. 

REQUIREMENTS . 

QUALITY ASSURANCE PROVISIONS 
PREPARATION FOR DELIVERY ... 
NOTES . 


iv 








Apollo G & N Specification 
PS-1000288“H 

00 May 10 6 3 - 
26 Nov. 1963 


PROCUREMENT SPECIFICATION 
SATURABLE REACTOR 
(APOLLO IMU BLOWER SPEED CONTROL) 


1 . 


1.1 


2 . 


2.1 


SCOPE 

Control) hereinafter called saturable reactor. 


APPLICABLE DOCUMENTS 

The following documents of th ® ls ® u ® 
invitation for bids form a part of t.J.- 
extent specified herein. 


effect on the date of 
specification to the 


SPECIFICATIONS 


Military 

MIL-T-27 

MIL-P-116 

MIL-E-17555 


Transformers and Inductors (Audio, Power, 
and Pulse) 


Preservation, Methods of 


lectronic and Electrical Equipment and 
associated Repair Parts, Preparation for 
. ..._ «<< 


Apollo Q & N 
ND-1002023 

ND-1002047 
ND-1015^0^ 

ND-1002019 


rocedure for Serialization of Components, 
ssemblies, etc., for Apollo Guidance and 


Qualification Specification, Transformers 
and Inductors. 


'neral Specification, Configuration, Pro- 
;ss and Quality Control Requirementsfor 
appllers of High Reliability Articles for 
„_ net F.rmiDment 


Marking. General Specification for 


1 


Apollo G & N Specification 
PS-1000288—1 
■3 0 May 1P S 3 - 
21 Aug 1903 


STANDARDS 

Federal 

FED-STD-595 

Military 

MIL-STD-202 


Colors 

Test Mechods for Electronic and 
Electr cal Component Parts 


DRAWINGS 


Apollo 0 & N 
1000288 


2.2 


3. 


3.1 


3.2 

3.2. 


Saturable Reactor (Apollo IMU Blower 
Speed Control) 


fPonies of specifications, standards, drawings, and publications 
in ejection with specific Procurement 
functions should be obtained from tne procuring activity 
directed by the contracting officer). 

CONFLICTING REQUIREMENTS, an the event of conflict between thC 
requirements of this specification and “peclflcatlons 

and drawings cited herein, resolution must be ob ** llied from 
the MIT APOLLO Management Office via the purchaser. 

REQUIREMENTS 

The requirements of this specification are classified into two 
headings: 

General Requirements which are defined in paragraph 
3.2 and Performance and Product Characteristics which 
are defined In paragraph 3.3. 

DESCRIPTION. The unit shall be ^ s aturable factor power output 

and bias windings. 

GENERAL REQUIREMENTS 

Qualification Testing. When specified by the purchase^ a 

«.-S2S-*!8ra!;- 

grar jsa&rja s 

of the supplier as determined by NASA or the purchaser. 


2 


Apollo G & N Specification 

FS-100U288-H 

25 Nov. 1953 

Further prod ictior. of the item by the supplier prior to approval of the 
purchaser or xhe comrletior of qualification tests shall be at the supplier’s 
risk. ' Requalification will be required at the discretion of NASA or the 
purchaser in the event that. 8/ the supplier has modified the item , b) the 
supplier has instituted a change in the material used cr in his processing, 
and c ) the specification requirements for the item have been amerded or 
revised sufficiently to affect the character of the item. 

The qualification tests will be conducted in accordance with the procedures 
specified ir Section 4. 

3. 2. 2 Fequalificatio n Te sting. When specified by the procuring activity, the 

suT)nTieF sHaT■ subnut one or more saturable reactors to be selected from 
eacn products lot by the procuring activity for submission to a designated 
testing activity to determine compliance of the sample(s) with the require¬ 
ments of the contract, specification, and drawings. 

3 2 3 Materials and Construction. The materials used in fabricating the saturable 
reactor*s r aTTT^iTTi trlbt *Jcordancu with the applicable drawings and speci¬ 
fications referenced herein. Substitute materials shall be selected with such 
quaiitv as to ens re that the equipment will meet the requirements of this 
specification and will be subject ter prior approval of the procuring activity. 

2 2 4 Weirht, Dimensions, Finish, and Mar king . The weight, dimensions, finish, 

a^Tn^GTTE^satumlbleTeactor shall comply with the requirements 
specified herein or on the applicable drawings. 

3. 2 . 4 . 1 Weight. Tie v/eight of the saturable reactor shall not exceed l. 5 ounces. 

3. 2. 4. 2 Finisn. Finish shall be as specified on the applicable drawing. 

3. 2. 4. 3 Marking. Marking shall be in accordance with Specifications MIL-T-27 and 
ar.d as specified on the applica ale drawing. 

3 2 5 Serial Numbers. Each saturable reactor identified by General Arrangement 

Tor A 3 semblyF.Drawing shall be identified by a serial number assigned m 
accordance wi.h Specification ND-1002u23. 

3 2 f, Workmanship. The fabrication and finish of the saturacle reactor, its 
assemblies, subassemblies, and parts shall be such as to produce a unit 
free from any defect trat would affeer. proper functioning in service. 


3 . 2.7 


3 . 2.8 

3 . 2 . 8 . 1 


3 . 2 . 8 . 2 


3.3 


3 . 3 . 1 


3 . 3 . 1 . 1 


3 . 3 . 1.2 


Apollo G&N Specification 
PS-10000288-H 
30 May 10 6 3 - 

"M A in 


26 No'/. 10^3 

Warranty A warranty shall provide for the supplier to 
remedy "by correction or replacement any component or 
end item found to be defective in material or workmanship 
not later than six (6) months after acceptance. 


The allowability of the cost of any such correction or replace- 
mpnt shall be determined as provided in the clauses of 
appropriate contract entitled "Allowable Cost, Fixed Fee and 
Payment", and "Inspection and Correction of Defects . 


Service Lif e 

Operating Life The saturable reactor design is intended to 
meet performance speciucations for at least 20,000 hours 
of operation, excluding the supplier's test time of the completed 


Shelf Life The saturable reactor design is intended to have a 
shelf life of at least 5 years, without operation, at ambient 
room temperature after final acceptance at the supplier s 
plant. 


PERFORMANCE AND PRODUCT CHARACTERISTICS. 

The following requirements are stated to inform the supplier of 
specific characteristics and of the goals that were considered in 
the design. Inclusion of this information shall not be construed 
by the supplier as authorization to modify the design. 


If the design of any part is not completely specified by the con¬ 
tractual documents, the supplier may submit a suggested design 
document for approval which will support these requirements. 


If, in the opinion of the supplier, any design or testing shall 
impose undue time delay or expense, he shall so state, in detail, 
in a counter-proposal, substantiating all contributing factors 
when submitting a bid, proposal, proposal, or change request 
in connection with this specification. 


Requests for changes or deviations to this specification or to 
applicable drawings, specifications, publications, materials, or 
processes specified herein shall be accompanied by written 
justification. 


Functional Requirements 

Winding Resista nces. DC resistance of the windings shall be as 
specified on Apollo G&N Drawing 10000288. 

Dielectric Strength. The saturable reactor shall exhibit no 
evidence of breakdown when subjected to a 500V rms voltage. 


Insulation Resistance. The insulation resistance of the saturable reactor 
shall be 100 megohms minimum* 


4 


Apollo G & N Specification 
PS-10002^8 - J 
4 )0 May 10 3 9 - 
25 Aug 1964 


3.3.1.4 

3.3.2 

3.3.3 

3.3.3.1 

3.3.3.2 

3.3.3.3 

3.3.3.4 

3.3.3.5 

3.3.3.6 

3.3.3.7 

3.3.3.9 


Performance. Linear output 'range and linearity of output shail be 
as spec ' lTi ed in Figure 1 when the saturable reactor is tested in . 
accordance with 4.2.7. 

Rnvl-ronraental Requirements. The saturable re_aeto«i_shan be capable 
of meeting the requirements of Specification ND-1002047, excep- 
that the Temperature Cycling teat shall be non-operating only. 

Design Requirements . 

Interchangeability. Unless otherwise specified, the saturable 
reactor and its ‘component parts shall be physically and functionally 
interchangeable without selection or fitting. 

Reliability. The saturable reactor shall be capable of °P e £®^ ng 
a minimuhTof 20,000 consecutive hours without maintenance under 
any combinations of conditions specified herein and shall have a 
maximum failure rate of 0.5 failures per 1,000,000. 


>ression. The suppression of radio noise 
be consi dered in the design of the saturable 


Radio Inte rference Suppression. 
and 'Interference shall be consi 
reactor. 

Flammable Materials. Materials which may be ignited^orjausejn 
explosion shall ' noE be used for construction applications where 
sparking or arcing could cause ignition. Materials which 
inadvertently support combustion shall not be used. 
impregnating, potting or embedding compounds, when enclosed 1 
fire-resistant containers, shall be acceptable. 

Materials. Materials which produce harmful toxic ef fec *®_ 4 _ 
during serv ice*" u sage shall not be used. Where a suitable nontoxic 
material Is not available, preventive measures shall be P™^ d ® d * 
subject to the approval of NASA. Materials wh ® n lK n * ted * 

produce toxic substances or vapors shall be avoided whenever 
practicable. 

PnRt.nhi e Materials. Materials which are unstable or become un- _ 
stable to the extent that they emit or deposit corrosive substances 
capable of causing corrosion or producing electrical leakage Paths 
within an assembly under possible operating and storage conditions 
shall not be used during manufacture or recommended for use during 
maintenance. 

Corrosion. Moisture, and y ung us -Resistant Materials. Materials 
shall be selected for noncorrosive and nonhygroscoplc character¬ 
istics and ability to resist the effects of corrosion, moisture 
and fungus. Preference shall be given to materials with Inherent 
fungus resistance rather than reliance upon the application o r 
surface fungistatic or fungicidal treatments. 

Dissimilar Metals. The use of dissimilar metals shall beavolded 
wheneverpractT cable. Magnesium shall not be used «?ept with the 
prior approval of the procuring agency or when so called -or on 
the applicable Apollo G le N drawings. 


5 

L 


Apollo G & U Specification 
PS-1000288-P 
ei Aug vj*y 
* Sept 19*3 



CONTROL CURRENT - AMPERES DC 


30V * ±$ BIAS 

Input: 29.4V rms - \1» 
Load: 59 ohnu* - 
Freq: 800 cps - 1$ 
Ambient Temp: 7CP±5° P 


25V * 1% BIAS 
Input: 26.6V rms * rf l# 

P 


Load: 73 ohms - *5 
Freq: BOO cps ±1> 
Ambient Temp: 7C Pf 5° 


Figure 1. 


Linear Output Range and Linearity 





Apollo G & N Specification 
PS-inonp 8 Q . -E 
80 May lO fr fr 
21 A ig 1963 


4. QUALITY ASSURANCE PROVISIONS 

4 1 GENERAL, Unless otherwise specified herein, the supplier is res¬ 
ponsible for the performance of all inspection requirements 
to submission for NASA inspection and acceptance. Except as other¬ 
wise specified, the supplier may utilize his own facilities or any 
commercial laboratory acceptable to NASA. Inspection records of 
the examinations and tests shall be kept complete and a ^ilable 
to NASA as specified in the contract or order. The supplier shall 
conform to Class 1 of Specification ND-1015404. 

4.1.1 Acceptance Tests. These tests shall be accomplished on each_ 

saturab 1e r e ac To r being submitted for acceptance under the contract. 

Acceptance test data on each unit accepted must accompany 

to the purchaser. Acceptance tests shall be wl £ n ®®®®^ 

nizant government inspector, a representative of the P u £?£ a ®®£» 

as the purchaser may direct in the procurement order. These tests 

are detailed in 4.2. Failure of the saturable 

with these requirements shall result in rejection of the item. 

4.1.? Qualification and Requalific ation Tests . Qualification and ^Re- 
qualiiTca TT o n te'sts~WalT^e accomplisnea at a NnoA aesignctcd 
activity. These tests, as outlined in 4.3, shall be conducted 
after the award of the contract to determine that the production 
will meet all requirements of this specification. Acceptance 
shall be based on no defects in the saturable reactor. 

Failure of the saturable reactor to comply with these retirements 
shall result in the rejection of the lot or the cessation of pro¬ 
duction, as determined by the purchaser. 

4.2 ACCEPTANCE TESTS 

4 ? 1 Test Conditions. Unless otherwise specified herein, the saturable 
* * waotw Bhair Tfc subjected to tests under the following ambient 
conditions s 


(a) Temperature 

(b) Relative Humidity 


25 + 10 0 

Not more than 90$ 


4.2.2 


(c) Barometric Pressure 28 to 3t Inches Hg. 

Test Power. The following electrical input, as measured at the 
Incut §f l h e unit under tSst. is necessary for testing this item: 
26^6 to 29.4V rms adjustable, 800 cps +1 percent, single phase, 

5 percent maximum harmonic distortion/T.0 va maximum power. 


7 


Apollo G !t N Specification 

PS-10002U8-H 

26 Nov. 19 63 


4 2 3 Visual and Mechanical Inspection. A comprehensive inspection shall oe 
rna-3c drtnTsaTurcEIe reactor tolTe+ermine the extent of compliance wife 
the requirements oi this specification and the applicable Apollo G & N 
drawing specified in Section 2 and shall at least include determination on the 
following: 

a) Size, dimension, tolerance, weight, appearance and marKings. 

b) Adequacv of materials, parts, and subassemblies; compliance 
with specific ratings, and conformance to applicable specifications. 

c) Finish, coatings, construction, markings, and nameplates, as 
applicable. 

d) Wiring, cabling, welding, soldering, color coding, and terminals, 

as applicable. 

e) Workmanship and cleanup. 

4. 2. 4 Winding Resistances. Winding resistances shall be tested by using 
method 303 of MlL^STD-202 and shall be as specified on Apollo G N 
di awing 1000288. 

4 2. 5 Dielectric Strength. Dielectric strength shall be checked by applying a ^ 

5CCV rms, 60 cps'voltage between each terminal and the case and a 200 V rins, 
60 cps (100 K source impedance) voltage between the terminals specified in 
Table I. The leakage current shall not exceed !. 0 ma. This test shall be 
conducted in accordance with method 201 of MIL-STD-202. 


Table I. Dielectric Strength and Insulation Resistance 


Between Terminals 

Between Terminals 

7 arid 1 

1 and 2 

7 and 2 

1 and 5 

7 and 5 

2 and 5 


4 2 S Insulation Resistance. Insulation resistance shall be checked by applying a 
300 vdc voltage (current limited to 6^amp) between each terminal and tne 
case and between the terminals specified in Table I. The minimum acceptable 
resistance shall be 100 megohms. This test shall be conducted in accordance 
with method 302 of MIL.-STD-202. 

4 2 7 Performance. With the test setup specified in Figure 2, linear output range 
and linearity"of output shall be checked by performing the following steps m 
the sequence indicated: 

a) Set switch S-l at position "l”. 

b) Adjust load resistor Rr to 73 ohms ±0.1 percent. 

c) Adjust line voltage to 26. 6 V rms ± 1 percent. 

d) Adjust frequency of line voltage to 800 cos 1 percent. 

e) Adjust ambient temperature to 70 ± 5 F. 


8 


Apollo GAN Specification 
PS-1000288-Ai 
8 0 May lO Sfr 
a July 1^63 - 
ai Aug losa- 

26 Nov. 1963 



800 CPS + 1% 


Total resistance of resistor "Re" 
plus ammeter "A" * 15. 5 ohmrf*+ 1% 

"A" = 0-2 DC AMMETER, 0.1%ACCURAQf 

"V H .« J. FLUKE AC DIFFERENTIAL 
VOLTMETER MODEL 803 
OR EQUIVALENT 

"IL M * 280 ohms - 0.1%. 3W min., 

® wirewound resistor 


Figure 2. Test Setup 


Apollo G & N Specification 
PS-1000 288-J 
SO l i u i . 1068— 

25 Aug. 1964 


4.3 

4.4 


f) Adjust bias voltage to 25 V ±1 percent. 


2 > 


li) 

i) 

j) 

k) 


( E tabiliration5 the output current shall be within the Un.it. spectftcd 
in Figure 1. 

Th 7 pa 

zs sar.ffjsss - s • 

specified in Figure 1. 

Insert load resistor (Rl> » f S9 oh 1118 ± °- 1 percent ‘ 

Adjust Une voltage to 29.4 V rms 11 percent. 
m > Adjust frequency of line voltage to 800 cps ± 1 percent, 
n) Adjust bias voltage to 30 V ±1 percent. 

- *^^S&!aSSBZS'-’£S' 

specified in Figure 1. 

asssass m as saBasa*' " Z 

in Figure 1. . 

-max IFICATION AND REQUALIFICATION TESTS. Qualification and re- 

SIID-1002047Z (Txt’ept^hat'the^Temperatur^Cycling'tes't^hall^xe performed 

R 0 ELW P BIUW. 0nl The cal^eff” tal^ 

specification are design objectiv . ^ P for ;he sup piier to dernon- 

st^^hi^corrpU^ce wtth tire MquirernenL ^\railable*'fo I r e^ablZshirg the 

ment of the reliability objectives specified. 


P> 

q> 


10 


Apollo G & N Specification 
PS-1 000288"A 
29 May 1963 


5. 


5.1 


5.1.1 


5.1.1.1 

5.1.1.2 


5.2 


5.3 


5.4 


6 . 


PREPARATION FOR DELIVERY 

PRESERVATION AND PACKAGING. -The saturable reactor shall be pre¬ 
served and packaged in accordance with Specification MIL-E-17555, 
level B, as specified in the contract or purchase order. 

Level B (Limited Military Packaging). Level B packaging is that 
which will a f for d adequate protection against damage during 
multiple domestic shipments, handling, and covered storage. 

Cleaning. Cleaning for Level B preservation and packaging shall 
be in a ccordance with method C-l of Specification MIL-P-llb. 


Unit Protection. The saturable reactor shall be individually 
afforded unit' protection in accordance with method III of 
Specification MIL-P-116. In addition, equipment packaged for 
level B protection shall be sealed against water and dust by means 
of suitable wrapping. 

REPAIR PARTS. Repair parts shall have preservation and packaging 
per the applicable repair parts list and its packaging supplement. 

PACKING. The equipment shall be packed in accordance with 
Specification MIL-E-17555, level B. 

MARKING. In addition to any special marking required by the 
contract or order, the marking of unit, interior packages, and 
exterior shipping containers shall be in accordance with level B 
of Specification MIL-E-17555* 


NOTES. 

NOTICES When NASA drawings, specifications, and other data are 
used for any purpose other than in connection with a definitely 
related NASA procurement operation, NASA thereby incurs no 
responsibility nor any obligation whatsoever, and the fact that 
NASA may have formulated, furnished, or in any way supplied the 
said drawings, specifications, or other data is not to be re- 
garded by implication or otherwise as in any manner licensing the 
holder or any other person or corporation, or co ? ve £;* g 
or pemission to manufacture, use or sell any patented invention 
that may in any way be related thereto. 


11 


APOLLO G&N Specification 
PS1000288 K 
Original Issue Date: 
Release Authority: TDRR 
Class Release 


PROCUREMENT SPECIFICATION 
FOR 

SATURABLE REACTOR 
(APOLLO IMU BLOWER SPEED CONTROL) 


(continued) 

Record of Revisions 


Date 

Revision 

Letter 

TDRR 

No. 

Pages 

Revised 

Approvals 

MIT 

NASA 

11 /12/6 

l K 

14101 

6 V ^ 

WK 

WJR 




















































1 




This specification consists of page 1 to 11 : nclusive. 


APPROVALS 


T 


ACSP 


1-1 


NASA/MSC 


MIT/IL 















Apollo G & If Specification 
PS-1000288- K 

i -*u," 1 -■ .3 



CONTROL CURRENT - AMPERES DC 


30V * 1 i BIAS 

Input: 29.4V nos - 1 $ 
Load: 59 ohms X l£ 
Freq: 800 cps - 1$ 
Ambient Temp: 7 CP- 3 0 F 


25V * 1* BIAS 

Input: 26.6V ras * ljl 
Load: 73 ohms t x 5 
Freq: 800 cps i 1% 
Ambient Temp: 7CP^5° F 


Figure 1. 


Linear Output Range and Linearity 





Apollo G & N Specification 
PS-1000288 - X 


PROCUREMENT SPECIFICATION 
SATURABLE REACTOR 
(APOLLO IMU BLOWER SPEED CONTROL) 


1 . 


1.1 


2 . 


2.1 


SCOPE 

SCOPE. This specification establishes the requirements for the 
procurement of the Saturable Reactor (Apollo IMU Blower Speed 
Control) hereinafter called saturable reactor. 

APPLICABLE DOCUMENTS 

The following documents of the Issue In effect on the date of 
invitation for bids form a part of this specification to the 
extent specified herein. 

SPECIFICATIONS 


Military 


MIL-T-27 


MIL-P-116 

MIL-E-17555 

Apollo G & N 

ND-1002023 


ND-1002069 
ND-1015^04 


ND-1002019 


Transformers and Inductors (Audio, Power, 
and Puls:) 

Preservation, Methods of 

Electronic and Electrical Equipment and 
Associated Repair Parts, Preparation for 
Delivery of 


Procedure for Serialization of Components, 
Assemblies, etc., for Apollo Guidance and 
Navigation Equipment 

Qualification Specification, Magnetic 
Amplifiers”. 

General Specification, Configuration, Pro¬ 
cess and Quality Control Requirements for 
Suppliers of High Reliability Articles for 
Use in Spacecraft and Supporting Equipment 

Marking, General Specification for 


1 



Aoollo G & N Specification 
PS-1000PB8- 

Class A Release 
TDRR 01266 
15 May 1963 


PROCUREMENT SPECIFICATION 
FOR 

SATURABLE REACTOR 
(APOLLO IMU BLOWER SPEED CONTROL) 


Record of Revisions 



(continued) 



APOLLO G6N Specification 
PS1000288 L 

Original Issue Date: IS May 1963 
Release Authority: TDRR 01266 
Class A Release 


PROCUREMENT SPECIFICATION 
FOR 

SATURABLE REACTOR 
(APOLLO IMU BLOWER SPEED CONTROL) 


(continued) 


Record of Revisions 


Date 

Revision 

Letter 

TDRR 

No. 

Pages 

Revised 

Approvals 

MIT 

NASA 

11/12/6 

% K 

14101 

6 'r .... 

WK 

WJR 


I, 

MM 

1. 6. 10 

WK 

W JR 


















































This specification consists of page 1 to 11 inclusive. 


APPROVALS 


NASA/MSC 


MIT/I L 


ACSP 


a 

i-A 















Apollo G & N Specification 

PS-1000288 -L 


3.3.1.4 


3.3.2 

3.3.3 
3.3.3.1 


3.3.3.2 


3.3.3.3 

3.3.3.4 


3.3.3.5 


3.3.3.6 


3.3.3.7 


3.3.3.8 


Performance. Linear output range and linearity of output shall be 
as specfiT ed in Figure 1 when the saturable reactor is tested in 
accordance with 4.2.7. 

Environmental Requirements. The saturable reactow shall be capable 
of mee't'Ing t'he* requirements of Specification ND-1002C59„ except 
that the Temperature Cycling test shall be non-operating only. 

Design Requirements . 

Interchangeability. Unless otherwise specified, the saturable 
reactor and l ' fs " c o m ponent parts shall be physically and functionally 
Interchangeable without selection or fitting. 

Reliability. The saturable reactor shall be capable of operating 
a mInImum”of 20,000 consecutive hours without maintenance under 
any combinations of conditions specified herein and shall have a 
maximum failure rate of 0.5 failures per 1,000,000. 

Radio Interference Suppression. The suppression of radio noise 
and Interference" shall cc considered In the design of the saturable 
reactor. 

Flammable Materials. Materials which may be ignited or cause^an 
explosion shall" no E be used for construction applications where 
sparking or arcing could cause Ignition. Materials which 
inadvertently support combustion shall not be used. Flammable 
impregnating, potting or embedding compounds, when enclosed in 
fire-resistant containers, shall be acceptable. 


Materials. Materials which produce harmful toxic ef fect ®__, _ 
during service usage shall not be used. Where a suitable nontoxic 
material is not available, preventive measures shall be provided, 
subject to the approval of NASA. Materials which, when ignited, 
produce toxic substances or vapors shall be avoided whenever 
practicable. 


Unstable Materials. Materials which are unstable or become un- 
stable to the"extent that they emit or deposit corrosive substances 
capable of causing corrosion or producing electrical leakage paths 
within an assembly under possible operating and storage conditions 
shall not be used during manufacture or recommended for use during 
maintenance. 


Corrosion. Moisture, and *ungus-Res.lstant Materials . Materials 
shall b" selected for noncorrosive and nonhygroscopic character¬ 
istics and ability to resist the effects of corrosion, moisture 
and fungus. Preference shall be given to materials with inherent 
fungus resistance rather than reliance upon the application o^ 
surface fungistatic or fungicidal treatments. 


Dissimilar Metals. The use of dissimilar metals shall be avoided 
whenever practicable. Magnesium shall not be used except^wlth the 
prior approval of the procuring agency or when so called .or on 
the applicable Apollo 3 1 N drawings. 


5 

*L 



Apollo G & N Specification 
PS-10002b8-L 


4.3 


4.4 


f) Adjust bias voltage to 2b V ±1 percent. 

2 > 


it CPUS* Ultio YW* *- * 

stabilization) l *the output current shall be within the limits specified 
in Figure 1. 


The output 


h> Current < shali*be 1 wlthin^the^bmit s a 8p^ifte^n C Ftgu , re n i. ^ ' 

» ^^fas^tr^t ‘ 

specified in Figure 1. 

j) Insert load resistor <R L > of *9 ohrr.s ±0.1 percent. 

k) Adjust Une voltage to 29.4 V rras * 1 percent. 

m> Adjust frequency of line voltage to 800 cps ± 1 percent, 
n) Adjust bias voltage to 30 V * 1 percent. 

specified in Figure 1. 

in Figure 1. • , . 

CHAT IFICATION AND REQUALIFICATION TESTS. Qualification and re- 

SiD-iootosS? exceV^t'l^Tem,^^^ 

reliability re 1—s^^ cal^dTr KT" 
specification aredesignobjectiv . £ fo r ihe y supplier to demon¬ 

procurement cortract, it shall "<* “V t T y he supp iier shall furnish the 
strate his compliance with the r q • llable for establishing the 

purchaser or NASA such data as ne ^ -have »"“* accumu lated to 

current reliability of these crits Adait onal ^aU ^ 1 ^ Qther 

ment of the reliability objectives specified. 


10 















































1 


Suppliers of High Reliability Articles for 
Use in Spacecraft and Supporting Equipment 









































































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| REVISIONS || 

ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL || 


A 

2.000 MTG HOLE DIM WAS 1.875 





_b: 

1.250 DIM WAS L125 . 

2 500 •• _ •• 2-250 ."" 


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NOTES 

I. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 
Z. BREAK ALL SHARP EDGES -^1 
S 63/ MACHINE FINISH ALL OVER 

_4:~aut radii ;S5S. r unless otherwise specified 


DRAWING NO.,REVISION LETTER AND 
MANUFACTURERS SYMBOL PER ND 1002019 ~ 

6. ANODIC COAT PER MIL-A-BC.Z5 TTPE 1, CLEAR 

7. CONFIGURATION < DIMENSIONS CONTROLLED BY Ti r LlI 

: xcd mhoi-oioos-hg : .: •• •—:~ 


QTY. 

NOMENCLATURE 

PART OR 

SPECIFICATION 

MATERIAL 

FINO 

REQO. 

OR DESCRIPTION 

IDENTIFYING NO. 

OR NOTES 

NO. 


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1001591 


application 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

- ±.005 - 


DO NOT SCALE THIS DRAWING 


MATERIAL: fcOGl ,T Q> 

ALT SPEC QQ-A-327B 


LIST OF PARTS AND MATERIALS 


M 1 T 

INSTRUMENTATION 

CONTRACT 

NAS 9153 1 

LAB 

"SatT 

APPROVED 

MwHf 


CHECKED 

ft 


DRAWN ^ \ 


S-2J-63 

fs 


MIT/IL APPROVAL 

DATE 




BRACKET 


{coolant line} 


SCALE 

e/i 


1 


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1 * 1 -* ! 1 1 * j 


0 I 2 

I PHOTOGRAPHIC SCALE ONLY 

s _----- 


UNIT WT. 


CODE IDENT. 


- MIT "- 

INSTRUM ENT ATION 
LABORATORY 

CAwmoaK. Mam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 


1000292 . 


SHEET ] OF \ 


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3 


2 


ZONE SYM 


REVISIONS TPRK OIBO^ 


DESCRIPTION I DATE I APPROVAL 


CHARACTERS* TO BEL 
3 PLACES 


4 PLACES 


CHARACTERS TO BE. ‘Jlj^ 
7 PLACES 


-•120 DIA 
.130 

A HOLES 

1^.010 D1A.I 


2.750 BSC 


isa 

ir 


Unertial Meas. Unit 

FOR APOLLO G t N SYSTEM 

DESIGNED BY 

M.IT INSTRUMENTATION LAB 


MFD.BY p 
NASA-MSC- 
NASA NO 


:o7z 

.052 

BORDER 



L .557 

.567“ 

.870__ 

.880 

363___ 

373 

_ I.2GO__ 

1.270 


m .432 \ m _1.260 _ 

.442 J.27Q 

. ..._1.731 __ 

1.80V 

__2.026_ 

USIQXE5 2.0 3G 

1. INTERPRET DRAWING IN ACCORDANCE WITH M1L-D-70327 

2. PLATE MUST CONFORM TO REQUIREMENT S AS OUT LINED IN 
MIL-P-15024, TYPE A OR TYPE H 

3. ANODI2E PER MIL-A-BG25,TYPE 2 EXCEPT EDGES 

4. BACKGROUND TO BE BLACK, MARKING AND LETTERING-TO BE 
NATURAL. METAL r 

5. WHERE LOCATING? DIMENSIONS ARE NOT SHOWN, CHARACTERS._ 

1 SHALE BE SYMETRICALL.Y POSITlONED AT THE INDICATED LOCAT ION 
G. IDENTIFY! USING DRAWING NO.,REVISION LETTER,AND MANUFACTURERS 
SYMBOL. PER MIL-STD-ISO ON FAR SIDE OF TV ATE 
7 FOR MASTER DRAWING „SEE. 1000237 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


_DLIOOOOOI DO NOT SCALE THIS DRAWING 

1000201 ~ DL10002(57 material AL ALY SH,ltOQ 

NEXT ASSY USED ON TEMP 

APPLICATION ALT : SPEC QQ-A-5GV,TO 


M 1 T 

INBTNU MENTATION LAB 
CONTRACT 


NAS 9-153 

"DATr 

AM»ROVEl£< 

Ufa***- 

7-l'b 3 

CHECK CO 



DRAWN 

R.S-.S. 


|t3 

^7^ 

MIT/IL 

APPROVAL 

DATE 

wiL 


4s- > 


LIST OF PARTS AND MATERIALS 

" PL/kT^.. 
IDENTIFICATION . 

ALE I UNIT WT. I CODE IDENT. 


INSTRUMENTATION 

LABORATORY 

CAMiMoti. Mam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1000296 

SHEET 1 OF | 






PHOTOGRAPHIC SCALE ONLY J J 












































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REVISIONS 

TPRR. o/s<=»2_ 

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DESCRIPTION 

| DATE | APPROVAL 


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1.937 

.REF 


Inertial Meas. Unit 

FOR APOLLO GEN SYSTEM 

DESIGNED BY 

M.I.T. INSTRUMENTATION LAB. 


12 


MFD. BY 
NASA - MSC - CO NT 
NASA NO. _ 

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±. 002 . 


1.000* 
PHOTO 
DIMENSION 


^ 1.002 


1 . 000 * 
PHOTO 
DIMENSION 


NOTE: 

!. THE ORIGINAL OF THIS DRAWING OR ANY REPRODUCTION THEREOF 
' SHALL fi>E MADE DT A METHOD OR PROCESS WHICH WILL INSURE 
DIMENSIONAL STABILITY AS AN ACCURATE TEMPLATE TO £>E 
USED TO PRODUCE IDENTIFICATION PLATE 1000296 


OTY. 

NOMENCLATURE 

PART OR 

SPECIFICATION 

MATERIAL 

FIND 

REQO. 

OR DESCRIPTION 

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OR NOTES 

NO. 


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UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGUS 








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MATERIAL 

NEXT ASSY 

USED ON 


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LIST OF PARTS AND MATERIALS 


M I T 

INSTRUMENTATION LAS 
CONTRACT 

NAS 9153 




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PHOTOGRAPHIC MASTER 


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UNIT WT. 


CODE I DENT. 


. MI T . "" "" 

INSTRUM ENTATION 
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Cawhipok. Mam. 


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SPACECRAFT CENTER 
HOUSTON TEXAS 


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1000297 


SHEET j OF r 


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(PRE HYDROEOKMED PATTERN LAYOUT ROLL-BONDED HEMISPHERICAL CASE'I 













































IJFLATION ~'J9E PASSAGE 



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?. INTERPRET LV.G IN ACCORDANCE W !T H D - ?C3D?. 

3. FNSH A^ FORMED UNLESS OTHERWISE SPECIFIED 

4. BREAK Ai i. SHARE EDGES ^tf ■ 

5. ORDER OE OPERATIONS: 

o. LOCATE HYDROFORMING BLANK PER 1000298 SHEET w l 
b. HYDROFORM 

C. ANNEAL PER MIL-H-6088C. BRINELL HARDNESS NOT TO EXCEED 35 (500-K 9 LOAD, 

10-MM BALL)CHECK AT INDICATED LOCATIONS 
d INFLATE ROLL BOND PASSAGES USING A DRV GAS AT 1000/1050 ^SIG INCREASE 
PRES' - FROMOPSIG TO 1000 PSIG ATAMA/IMUM RATE OF 500 PSIG/W1N. . 

e. DR!l. h r : IMMEDIATELY AFTER INFLATION TC RELIEVE SAS PRESSURE. 

f. «E-AMN£A TO RELIEVE WORK HARDENING PER MIL-H-6068. 

B A LINE (A-A) PASSING THROUGH THE CENTER OF'THE HEMISPHERE PERPENDICULAR TO 
[PLA NE A shall BE WITHIN ± OF INTERSECTING THE CENTER OF THE HYDRO FORMING 
BLANK (SEE SHEET**!) 



3 


2 


m 


QPR 07-3 


A 1 REVISED PER TDRR *1878 






2 



















PRICK PUNCH KT- 

•ggjDEEP r 
2 PLACES 1 


motes: 

l INTERPRET DRAWING IN ACCORDANCE WITH NML-D-70SZ7 
2. AVOID SCRATCHING MATERIAL WHEN LOCATING BLANK 
1 MATERIAL*. ROLL BONDED SHEET PER IOOI4GS 

(PRE HYDROFORMED PATTERN LAYOUT ROLL-BONDED HEMISPHERICAL CASE'i 


































































NOTES: 

1. MATERIAL : ROLL BOTCED SHEET PER 1004463. 

(PRE H/OROFORMED PATTERN LAYOUT ROLL-BONDED HEMSPHERICAL CASE) 

2. INTERPRET DWG IN ACCORDANCE WITH ML- D - 70327. 

3. FNSH AS FORMED UNLESS OTHERWISE SPECIFIED 

4. BREAK ALL SHARP EDGES ;§?| • 

3. OROEROF OPERATIONS: _ 

0 . LOCATE HYDROFORMING BLANK PER 1000298 SHEET 

B. HYDROFDRM 

C. ANNEAL PER MHL-H-6088C. BRINELL HARONESS NOT TO EXCEED 35 (500-K 9 LOAD, 
10-MM BALL)CHECK AT INDICATED LOCATIONS 

4 . INFLATE ROLL-BOND PASSAGES USING DISTILLED WATER 
' •. DRILL HOLES IMMEDIATELY AFTER INFLATION TO RELIEVE PRESSURE AND TO 
* FACILITATE FLUSHING 8 CLEANING OF THE PASSAGES 

f. FLUSH PASSAGES USING DISTILLED WATER,STEAM,THEN AIR. FURNACE DRY AT 
I50®F (*I0®F) FOR 2 H0URS(±I5MIN) 

*• A LINE (A-A) PASSING THROUGH THE CENTER OTTHE HEMISPHERE PERPENDICULAR TO 
(PLANET! SHALL BE WITHIN OF INTERSECTHK THE CENTER OF THE HYDROFORMING 

BLANK (SEE SHEETED ' . . a. 


7. IDENTIFY USING DWG NO.,REV LETTER AND MANUFACTURERS 
SYMBOL AT THE INDICATED LOCATION PER NQ 1002019 























































































































8 


6 


5 



1 






















































3 



2 








SURFACE 0 


NOTES: 

I. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MM.-D-7032 7 
Z. MATING FEMALE PLUG TO BE FULLY ENGAGED TO FIXTURE 
JtfOONTED CONNECTOR* PRIOR TO SILASTIC COATING BONG APPLIED 
% OUTSIDE SHELL (REF NOTE 2) TO BE COATED WITH MOLO RELEASE 
AGENT PER NO- 

* SURFACE A.B.C* 0, TO HAKE jOtO MIN THICK SILASTIC COATING PER NO 
5. SURFACE Eu» TO HAVE .095 THICK SILASTIC COATING PER NO* 


4 


3 


2 


1 


A 1 REVISED PER TDRR 1 l2-27G3| 


SURFACE A 



SURFACE B 


SURFACE C 


SEE NOTE 2 


100 1301 

MS35338-I 

1006783-13 


JIG SUB-ASSY 
WASHER, LOCK 
SCREW, BUTTON HD 
CONNECTOR, PLUG 


UNLESS OTHERWISE SPEC!RED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

* *.005 ± **■ 

DO NOT SCALE THIS DRAWING 
MATERIAL 


PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAS 


NOMENCLATURE OR 
DESCRIPTION 


MANNED SPACECRAFT CENTER 

HOUSTO N. TEXAS _ 

FIXTURE.POTTING ASS'Y 

PIP PREAMP 


ICOOE I DENT NO. I SIZE 


NEXT ASSY USED ON I FINAL FINISH” 




1001303 


1 SCALE 4/1 1*T 
























SEE NOTE 4 



B 


NOTES: 

I. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327 
Z. MATING FEMALE PLUG TO BE FULLY ENGAGED TO FIXTURE 
COUNTED CONNECTOR, PRIOR TO SILASTIC COATING BEING APPLIED 
% OUTSIDE SHELL (REF NOTE 4) TO BE COATED WITH MOLO RELEASE 
AGENT PER NO - 

' A SURFACE A.B.C. D, TO HAVE OIO MIN THICK SILASTIC COATING PER NO ~ 
- 9. SURFACE 6, TO HAVE .095 THICK SILASTIC COATING PER ND- 


i 


i 


SURFACE A 



- -SURFACE E 




T 


1 


wtvinoN* TORfT oonf 


| OATK | «WW»M. 


I: , 


M t 





2 


IBWHMllI 































FOR INFORMATION ONLY 


CLASS B RELEASE TOR I 


DATE 


■ C'SINK 85°±5° TOJIJDIA 


1 \ - 1872 

-4 U-.I87 

SECTION C-C 


"'l52 D,A ™ RU 

•g|0 X 45° CHAMFER FARSIDE 




SECTION D D 



^ BSC | 

_ 1562-4 

" t.563 1 


"'214 D,A ™ RU 


•S-.p 10Cl90V32 UNC 2B MOO THRU 
j[-v| MINOR D1A MOD 
C^INK 82°£l° '204 OJA 


l •‘STALL NEWTON INSERT KCL0-440 
t»WG ICOCI15-2 2REQ0 


unless ctherwhe vtcmtD 
- omtmtom me m mum 

_ TOLERANCES ON 

. ”3)05 l : 




MANNED SPACECRAFT CENTER 

HOUSTOH TUW 

FRAME 

VIB MOCK UP PSA VM 
HOLD DOWN METHOD*A* 

■ WNT Ml M21 I NMA MMN NO. 

j 1001305 




















13 EQUAL SPACE< 
TOTAL 2.600 00 ' 


±002 

AT .200 P'TCH 
TOL NON CUMULATIVE 




SECTION B-B 

SCALE 2/1 



FOR INFORMATION ONLY 

CLASS B RELEASE TOR Nag2iLZg_ MTE 

3 ^ 



SECTION C-C 



'lS2 °*A THRU 

020 x 45° CHAMFER FARSIQE 


/ 



SECTION D D 


|]| DIA THRU 


C BORE \l% OIA X .062 DEEP 
l&.COS DiAl 


INSTALL NEWTON INSERT KCL0-440 
DWG 1000115-2 2REQ0 


PART NO. I 


1 INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 

2 MATL 606I-T6AL/QQ-A-325 

3 FINISH BLACK ANODIZE MIL-A-8625 

4 SURFACE »2Sr UNLESS OTHERWISE SPECIFIED 

5 BREAK ALL SHARP EDGES 





APPLICATION 


SEE NOTE 3 

































3 


2 





"202 DIA THPJ $C'SINK 120* X Ilf DIA , 
PLUG TAP *3FPB X .437 DEEP, 6 HOLES 


INSTALL HELI-COIL INSERT (10-32) 3-9K3CN-0380, 

3/4 TO I 1/2 PITCH BELOW SURFACE, BREAK OFF DRIVING TANG 
6 REQ'D 


4.250 


3.000 


-3.500- 


•15.594 


! 76 DIA X 562 DEEP '4 C'SINK I20°xJ5|0IA,- 
PLUG TAP 2CPB X .375 DEEP 2 HOLES 
INSTALL HELI-COIL INSERT (8-32) 
#3585-2CN-0328 3/4 TO I 1/2 PITCH BELOW 
SURFACE BREAK OFF DRIVING TANG 
2 REQ’D 




FOR INFORMATION ONLY 


CLASS B RELEASE TDR No, qog-m 


DATE 


NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 

2. ALL CORNERS MUST BE .005 TO .015 R OR CHAMPER. '25/ 

3. UNLESS OTHERWISE SPECIFIED,- SURFACE ROUGHNESS MUST NOT EXCEED V 

4. MATERIAL : 2024-T4 ALUM. PER QQ-A-268 

5. FINISH: BLACK ANODIZE PER MIL-A-8625 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


M I T 

INSTRUMENTATION LAS 
Camnidw. Mam. 


MANNED SPACECRAFT CENTER 


HOUSTON, TEXAS 


*005 


DO NOT SCALE THIS DRAWING 
MATERIAL 

SEE NOTE NO. A 


MOUNTING PLATE 
‘ PSA VIB MOCKUP 


I HEAT TREATMENT 


NASA APPROVAL „ 


I CODE IDENT NO. SIZE 


NASA DRAWING NO. 




APPLICATION 


FINAL FINISH 

SEE NOTE NO. 5 


MIT APPROVAL \ 




1001316 


2 































































MOTICI - VMM WMMMUT MUW1HMS. ffCCIDICATMM. M OTNtR MT* 
MM MM Ml ANY MWOM OTNC* THAN IN CONNICTION WITH A MftNITIlV 
HLATtB NOVCNNNCNT PNOCMMNIAT ORCRATION. TNC MHITtO ITATKS ROVtRN- 
StNT TMMOT INC MRS NO MSDOHtUMLITY NON ANY OOLISATIONWIIATROfYIR: 

TACT THAT TNC OOVCNNNCNT HAT NAVt FOHHMLATSB. rNNWICMCO- ON 
10 TNC SAIN 00ACMN0C. SNCCIPICATIONS ON OTNCN BATA If 

„ _SCO NT INTLICATION ON OTMCNVISC AS IN Ai'Y HAHMCS 

UCCHOINO TNC NOtBCN ON ANT OTNCN PCROON ON CONDONATION. OR CONVCT- 
MO ANT NIONTS ON PCNNISSION TO NANMTACTMNC. MSC. O N SOU. ANT 
NATCNTCO INVCNTtON THAT NAT IN ANT OAT OC NR LA TOO TNCNCTO. 



L- -*| L—.062 


-250-»| 



1.000 


20 R MAX 
(4 PLACES) 


NOTES 


194 DIA THRU 


;DIA THRU 


30 

2 HOLES 


130 

(2 PLACES) 


I.INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327 

2.125/ ALL OVER 

3 . BREAK ALL SHARP EDGES’^ 

4 FINISH BLACK ANODfZE’ MIL-A-8625 


j-^266-^ 


.500 f | 

1 250 ‘1 


FOR INFORMATION ONLY 


1 . 1- 

k -4 



CLASS B RELEASE TDR Na ooano 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

* -U- *£>05 * Hh 

DO NOT SCALE THIS DRAWING 

mater,al 302 SST 

QQ-S-766 _ 

HEAT TREATMENT 


PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAS 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


. DATE1 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 

RETAINER,SCREW 
PSA VIB MOCK-UP 


I FINAL FINISH 


APPLICATION 


SEE NOTE 4 


NASA APPROVAL „ 


MIT APPROVAL 


3- JT-C** 



I CODE IDENT NO. I SIZE 


| SCALE 4/ I 


NASA DRAWING NO. 

1001317 

































































































































































ROLL-BOND VENDOR TO CRACK* 
INFLATE. LOCATING TUBE 
AS SHOWN IN SECTION A-A 



B 

r 



» B 


NOTES 

L INTERPRET DWG IN ACCORDANCE WITH M1L-D-TOS27 
ft. MATERIAL: ALUMINUM .TYPE. GOGI.DOUBLE THICKNESS .060+.004 
C.O30/OSC* (IN FABRICATING, ALUM TYPE GOGI _ 

.SHALL BE USED WITH BONDING SURFACES 

CLAD WITH ALUM TYPE UOQ\ ..... - • 

5. FINISH AS ROLLED 

«. ALL DIMENSIONS ARE SUBJECT TO ROLL-BOND FABRICATION TOLERANCES 
Al ROLLING TOLERANCES - t .ISO PER FOOT OF PATTERN LENGTH 
{ ft. OUT OF SQUARE-*.261 PER GINCHES OF PATTERN WIDTH 
! C. r AMBER -4 1/IG 

1 S. 0DENOTES SHEAR POINT . : - —Z - 

ft. MATERIAL SHALL BE ANNEALED (CDND 0) W RQLL-BCND VENDOR 
~7 SERPENTINE PATTERN NOT TO BE INFLATED 

ft IDENTIFY USING DWG NO. .REVISION LETTER % MANUFACTURES 
SYMBOL AT INDICATED LOCATION PER ND 002019 


t I00I4G3 

































































IOOI 4 G 3 





























































































A TT>*R llOAZ 


350 _ .12.0 

.340 ~ 7 * 130 

5)A.005T|r|/ 


TRANSITION PIECE 4-E 


•2§l 1 . 2.55 

.A95 / 1.243 


~-2DUKIF-aB 

_L C .005 ~ 

-B- 

SEE NOTE 4C 


BRAZE SEE NOTE 4- E 




£.7 O 1 ** 
*)AX)05TIr| 



_.2I8 
.223 PIA 
•)/LQO 5 TIR 


2 PLACES 
SEE NOTE 4-B 




'.375 MIN DEPTH FOUL THD 



jw *eo, 

005 TIR] 1#Bj005TIr| I 


♦5T*5* 

5 PLACES* 


- THESE SORFACES SHALL BE 
FREE FROM LONG\TUD\NAL 
AUO SPVRAU TOOL MARKS 


REQUIREMENTS: 

1. GENERAL 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIDEO IT MIL-D-70327. 

•. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IM NM015404, CLASS 3. 
C, ASSEMBLY SHALL BE PACKED A SHIPPED IM A MANNER THAT WILL: 

PREVENT CONTAMINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENDING OF THE NOSE TO A RADIUS OF LESS THAN 20 INCHES. 

0. IDENTIFY USING DRAWING NUMBER. REVISION LETTER AND MANUFACTURERS SYMBOL PER ND1002019. 

2. INSPECTION A ACCEPTANCE 

A. DIMENSIONS: AS SHOWN ON DRAWING 

B. CLEANLINESS: CONTAHINANT PARTICLES SHALL NOT EXCEED J50 MICRONS IN SIZE WHEN TESTED 

PER 

C. PRESSURE TEST: ASSEHiLY RUST NOT DEFORM WHEN INTERNALLY PRESSURIZED TO 90 PSIG WITH 
DISTILLED WATER. 

0. LEAK TEST: NAXIHUM LEAK RATE 5 X lO^STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
10 77.5 t .5 PSIG (PERFORMED AFTER PRESSURE TEST). 

5. DESIGN REQUIREMENTS 

A. MATERIAL: 

1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .00G/.008 WALL THICKNESS) 

2. BRAID: CRES CLASS 321 COND A PER QQ-S-7G3 

3. END FITTINGS: CRES CLASS 321 CONO A PER QQ-S-7G3 

4. TRANSITION PIECE: ALUMINUM GOBI TG PER QQ-A-325 

B. FINISH: 

1. STEEL SECTIONS; PASSIVATE PER MIL-F-14072 FIN E-300 


SPECIAL INSTRUCTIONS A INFORMATION 


1. REMOVE RURRS A BREAK SHARP EDGES .005/.015. 

2. MACHINE SURFACES ^ FINISH. 

WELDING: INERT WELD PER NIL-W-8G11 


C; THREADS MUST CONFORM TO MIL-S-7742. 

D. CONFIGURATION AND DIMENSIONS CONTROLLED BY ICO MHOI-01008-11G. 

E. BRAZING OF ALUMINUM TRANSITION PIECE TO STAINLESS END FITTING 
A PROPRIETORY PROCESS OF BI-BRAZE CORP. 

BROOKLYN 3*i N.Y. 


SE.ET NOTE B A 


LIST OF PARTS AND MATERIALS 

.. " . MfT . — 

- HOSE FLEXIBLE m VSSSSSS? m 
S5 WELDING ASSEMBLY T I 

SPACECRAFT TO OPTICS BASE .wcaSTcpn. 

g I -**• \»** ar \00\4 gT 

JT tMOT I Of I 


5 






















8 

1 

7 

6 

5 

_ * __ 

3 


2 


i _ 

1 




/. • 




(0 

TONE 

STM 

inscription 

I DATE | APPROVAL 








<ts> 


A 

TDRR 11042- 

> >64 M\(j$ 








\ 


B 

TDRR 14676 

I* 20 U>£ 



REQUIREMENTS: 

1. GENERAL 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY NIL-D-70327. 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN NM 015404, CLASS 5. 

C. ASSEMBLY SHALL BE PACKED A SHIPPED IN A MANNER THAT WILL: 

1| PREVENT CONTAMINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

D. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL PER ND1002019. 

2. INSPECTION A ACCEPTANCE 

A. DIMENSIONS: AS SHOWN ON DRAWING 

B. CLEANLINESS:REQUIREMENTS PER ND1002223 

C. PRESSURE TEST: ASSEMBLY MUST NOT PERMANENTLY DEFORM WHEN INTERNALLY PRESSURIZED 
TO 90 PSIG WITH DISTILLED WATER. 

D. LEAK TEST: MAXIMUM LEAK RATE 5 X 10-*>STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
TO 77 tj PSIG (PERFORMED AFTER PRESSURE TEST). 

3. DESIGN REQUIREMENTS 

A. MATERIAL: 

1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .006/.008 WALL THICKNESS) 

2. BRAID: CRES CLASS 321 COND A PER QQ-S-763 

3. END FITTINGS: CRES CLASS 321 COND A PER QQ-S-763 

4. TRANSITION PIECE: ALUMINUM 6061 T6 PER QQ-A-325 

B. FINISH: 

1. STEEL SECTIONS; PASSIVATE PER MIL-F-14072 FIN E-300 

C. CONFIGURATION: 

1. FLEXIBLE HOSE SHALL BE CAPABLE OF BENDING TO A 1» INSIDE RADIUS WITHOUT 
DAMAGE OR PERMANENT SET. 


4. SPECIAL INSTRUCTIONS & INFORMATION 
A. MACHINING: 

1. REMOVE BURRS A BREAK SHARP EDGES .005/.01S. 

2. MACHINE SURFACES ^ FINISH. 

I. MELDING: INERT WELD PER MIL-W-8611 
C. THREADS MUST CONFORM TO MIL-S-7742. 

0. CONFIGURATION AND DIMENSIONS CONTROLLED BY ICO MHOI-01008-116. 

,! IW KiMV TRi;*j\!?!ON PIECE 

■ -*«* a roop - »- 

E. JOINT MUST BE CAPABLE OF WITHSTAND INC A TEMPERATURE OF 500*F 
WITHOUT DEGRADATION. _ 


1001469 


NUT AMT I UKO 


SEE NOTE a A 


UST OF PARTS AND MATERIALS 


MIT 

IMKNTA1 

COMTMC _ 

NAS 9 193 f'BATY 




r MIT/H. APPROVAL | 


f MIT/M. APPROVAL 


HOSE FLEXIBLE 
WELDING ASSEMBLY" 

SPACECRAFT TO OPTICS BASE] 


-WTT- 


SPACECRAFT CENTER 

HOWTON lOAl 


1001466 


OATt 


SCALE 

I 


"iisf ' w r 


_— 

COOE IOENT. 


•MEET 

































6 


3 



L-350 Q 

.340°* 

|®A.005TIR 


~:.C40 «- 
060 

4 PLACES 




- 375 MIN DEPTH FULL THO. 


2. PLACES 
SEE NOTE 4 B 


X .2.2.3 m 
l®A^05TI 


-BRAZE SEE NOTE *E 


REQUIREMENTS: 

1. GENERAL ’ 

A. INTERPRET DRAWIN6 IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND101S404, CLASS 3. 

C. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT HILL: 

1. PREVENT CONTAMINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENDIN6 OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

B. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL PER ND1002014. 

2. INSPECTION AND ACCEPTANCE 

A. DIMENSIONS: AS SHOWN ON DRAWING. 

B. CLEANLINESS: CONTAMINANT PARTICLES SHALL NOT EXCEED 150 MICRONS IN SIZE WHEN TESTED 
PER 

C. PRESSURE TEST: ASSEMBLY MUST NOT DEFORM WHEN INTERNALLY PRESSURIZED TO 90 PSIG 
WITH DISTILLED WATER. 

D. LEAK TEST: MAXIMUM LEAK RATE 5 X 10"* STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
TO 77.5. t .5 PSIG (PERFORMED AFTER PRESSURE TEST) 

3. DESIGN REQUIREMENTS 

A. MATERIAL: S 

1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .006/.008 WALL THICKNESS). 

2. BRAID: CRES CLASS 321 COND A *R QQ-S-763. 

3. ENO Fin I MGS: CRES CUSS 321 COND A PER QQ-S-763. 

4. TRANSITION PIECE: ALUMINUM 6061 T6 PER QQ-A-325. 


1. STEEL SECTIONS; PASSIVATE PER NIL-F-14072 FIN E-300. 



DbjoostirI 


45**5* 

5 PLACES 


.6BO HEX 
.£70 



-THESE SURFACES SHALL BE 
FREE FROM LONGITUDINAL 
AND SPIRAL. TOOL MARKS 


4. SPECIAL INSTRUCTIONS AND INFORMATION 
A. MACHINING: 

1. REMOVE BURRS AND BREAK SHARP EDGES .005/.015. 

2. MACHINE SURFACES 'fy FINISH 
I. WELDING: INERT WELD PER MlL-W-B611. 

C. THREADS MUST CONFORM TO MIL-S-7742. 

D. CONFIGURATION ANO DIMENSIONS CONTROLLED BY ICD NH0I-0I008-I16. 

E. BRAZING OF ALUMINUM TRANSITION PIECE TO STAINLESS STEEL END 
FITTING A PROPRIETORY PROCESS OF BI-BRAZE CORP. 

BROOKLYN 31, N.Y. 


E 



•*»“' NOSE , FLEXIBLE "•"KKSCil! 

WELDING ASSY — 

!7Z 111 IUU TO SPACECRAFT | 


SEE NOTE 3A 


H 1001467 



I 



































TRANSITION PIECE 



REQUIREMENTS: 

1. GENERAL x 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED IT MIL-D-70327. 

SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN N01015404, CLASS 3. 

C. ASSEMBLY SHALL BE PACKED AND SNIPPED IN A MANNER THAT UILL: 

1. PREVENT CONTAMINATION OF TNE INTERNAL SURFACES. 

2. PREVENT BENDING OT THE HOSE 10 A RADIUS OF LESS THAN 20 INCHES. 

0. IDENTIFY USING DRAWING NUMBER. REVISION UTTER AND MANUFACTURER! SYMBOL PER NO100201V. 

2. INSPECTION AND ACCEPTANCE 

A. DIMENSIONS: AS SHOM ON DRAWING. 

B. CLEANLINESS'REQUIREMENTS PER ND1002223. 

* r 

C. PRESSURE TEST: ASSEMBLY MUST MOT PERMANENTLY DEFORM WHEN INTERNALLY PRESSURIZED TO 90 PSIO. 
WITH DISTILLED WATER. 

0. UAK TEST: MAXIMUM LEAK RATE 3 X 10~* STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
TO 77 +4 PSIG (PERFORMED AFTER PRESSURE TEST) 

3. DESIGN REQUIREMENTS 

A. MATERIAL: i 

FLEXIBLE TUBING: CUES; CLASS 321 (TRUE SEAMUSS OOG/.008 WALL THICKNESS). 

2. BRAID: CAES CLASS 321 COMO A PER QQ-S-7G3. 

3. END FITTIN6S: CRES CUSS 321 COHO A PER QQ-S-7G3. 

4 . TRANSITION PIECE: ALUMINUM GOBI TG PER QQ-A-32S. 

». FINISH: * 

1. STEEL SECTIONS; PASSIVATE PEA NIL-F-14072 FIN E-300. 


SPECIAL INSTRUCTIONS ANO INFORMATION 
A. MACHINING: 

1. REMOVE BURRS AND BREAK SHARP EDGES .005/.015. 

2. MACHINE SURFACES 'ty FINISH 
I. WELDING: INERT WELD PER MIL-W-0G11. 

C. THREADS MUST CONFORM TO MIL-S-7742. 

0. CONFIGURATION ANO DIMENSIONS CONTROLLED BY ICO MHOI-01000-11G. 

• - i. * •';.;rTonoK-‘ •* nr > r 

’ HROJKi. ‘ 31, . 


C. CONFIGURATION ' 

FLEXIBU HOSE SHALL BE CAPABU OF BENDING TO A 1* INSIDE RADIUS WITHOUT DAMAGE OR PERMANENT SET. 




























ions | trn 


i , i « I _ i -1 


3 




revisions OX63Q 


TDRR 11042 . 


REV/5ED PER TDRR IlSlC* 


U jA 


REVISED PER TOR* 


b-3rfe4|^ 


m 



REQUIREMENTS: 

1. GENERAL 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY NIL-D-70327. 

I. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND1015404, CLASS 3. 

C. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

1. PREVENT CONTAMINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENOING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

D. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL PER ND1002019. 

2. INSPECTION AND ACCEPTANCE 

A. DIMENSIONS: AS SHOWN ON DRAWING. 

B. CLEANLINESS REQUIREMENTS PER ND1002223. 


4. SPECIAL INSTRUCTIONS AND INFORMATION 

A. MACHINING: 

1. REMOVE BURRS AND BREAK SHARP EDGES .005/.01S. 

2. MACHINE SURFACES FINISH 

B. WELDING: INERT WELD PER MIL-W-8611. 

C. THREADS MUST CONFORM TO MIL-S-7742. 

D. CONFIGURATION AND DIMENSIONS CONTROLLED BY ICO MH0I-0I008-I16. 

E. JOINT MUST BE CAPABLE OF WITHSTANDING A TEMPERATURE 500°F 
WITHOUT DEGRADATION. 


4 


4 


4 



C. PRESSURE TEST: ASSEMBLY MUST NOT PERMANENTLY DEFORM WHEN INTERNALLY PRESSURIZED TO 90 PSI6. 

WITH DISTILLED WATER. 

D. LEAK TEST: MAXIMUM LEAK RATE 5 X 10-6 STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
TO 77 +4 PSIG (PERFORMED AFTER PRESSURE TEST) 

-0 

3. DESIGN REQUIREMENTS 

A. MATERIAL: 

1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .006/.008 WALL THICKNESS). 

2. BRAID: CRES CLASS 321 COND A PER QQ-S-763. 

3. END FITTINGS: CRES CLASS 321 COND A PER QQ-S-7G3. 

4. TRANSITION PIECE: ALUMINUM G061 TG PER QQ-A-325. 

B. FINISH: 

1. STEEL SECTIONS; PASSIVATE PER MIL-F-14072 FIN E-300. 

C. CONFIGURATION 

1. FLEXIBLE HOSE SHALL BE CAPABLE OF BENDING TO A 1- INSIDE RADIUS WITHOUT DAMAGE OR PERMANENT SET. 


a 


c 

c 


Qjy 1 NOMENCLATURE 1 PART OR 

1REQO. | OR DESCRIPTION | lOENTIfTINQ NO. 

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NO. | 

| LIST OF PARTS AND MATERIALS 1 

. — . l - 1 MIT "1 


1001470 


TOURANCn ON 

nwmu mmim 


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4 


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i r 


WELDING ASSY 

I.M.U. TO SPACECRAFT 


_XJ. JL - 

COOK IOCNT. 


LABORATORY 


SPACECRAFT CENTER 


1001467 


APPUCAHON 


SEE NOTE 3 A 


OAT! 


£-1 


UNIT 








































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.442. 

.4 32 * 


I ifc 





SEE NOTE 4 B 


THIS SURFACE TO BE FREE OF RADIAL 

AMD SPIRAL TOOL MARKS, ANKJULAR GROOVES UP TO 32 MICRO - INCHES 
MAX WILL BE FERMI3SABLE 


^—.812 WEX 
ACROSS FLATS 


.€59 *749 

.€61 -747 

DW ) .7.1 7 


— LEAVE SHARP “ 

-.003 MAX'" ~ ^ 

-.8125 - 20 UNEF-3A 
MAJOR DIA ■ 

PITCH DIA -T*™, 

MINOR DIA 7512-NOMINAL 


REQUIREMENTS: 


A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70J27. 

B. SUPPLIER SHALL COHFORH TO QUALITY ASSURAHCE PROVISIONS SPECIFIED IH HD1015404, CLASS 3. 

C. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

1. PREVENT CONTAMINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAH 20 INCHES. 

D. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL PER ND 1002019. 

INSPECTION AND ACCEPTANCE 

A. DIMENSIONS: AS SHOW ON DRAWING. 

B. CLEANLINESS: CONTAMINANT PARTICLES SHALL NOT EXCEED ISO MICRONS IN SIZE WHEN TESTED 

PER 1 

C. PRESSURE TEST: ASSEMBLY MUST NOT DEFORM WEN INTERNALLY PRESSURIZED TO 90 PSIG WITH 
DISTILLED WATER. 

D. LEAK TEST: MAXIMUM LEAK RATE 5 X 10"* STD CC/SEC OF HELIUM WEN INTERNALLY PRESSURIZED 

TO 77.5 t .5 PSIG (PERFORMED AFTER PRESSURE TEST). • 

DESIGN REQUIREMENTS 
A. MATERIAL: 

1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .00b/.008 HALL THICKNESS) 

2. BRAID: CRES CUSS 321 COND A PER QQ-S-7G3 

3. END FITTINGS: CRES CLASS 321 COND A PER QQ-S-7G3 
I. FINISH: PASSIVATE PER NIL-F-14072 FIN E-300 


SPECIAL INSTRUCTIONS AND INFORMATION 
A. MACHINING: 

1. REMOVE BURRS AND BREAK SHARP EDGES .005/.015. 

2. MACHINE SURFACES 12* FINISH 
D. WELDING: INERT WELD PER MlL-W-B611. 

C. CONFIGURATION AND DIMENSIONS CONTROLLED 
BY SEATON WILSON MFG. CO. 

BURBANK, CALIFORNIA 


wcrss r rrr .vj ; sr cnm 



UST OF PARTS AMD MATERIALS 

HOSE FLEXIBLE 
WELDING ASSY 

OPTICS BASE TO LMU 
SPECIFICATION CONTROL DWG 


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-.375 MIN DEPTH FULL THD. 


. 6 6o MPX 

j) C..005 TIrI 1# C.005 TIrI .&70 



SEE NOTE 4 B 


THIS SURFACE TO BE FREE OF RADIAL 

AND SPIRAL TOOL MARKS, ANNULAR GROOVES UP TO 32 MICRO - INCHES 
MAX WILL BE FERM/SSABLE 




45* i 5* 

5 PLACES 


-THESE SURFACES SHALL BE 
FREE FROM LON6\TUOINAL 
AND SPIRAL TOOL MARKS 



REQUIREMENTS: 

1. GENERAL 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND1015404. CLASS 3. 

C. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

1. PREVENT COMTAHINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENDING OF THE NOSE TO A RADIUS OF LESS THAN 20 INCHES. 

0. IDENTIFY USING DRAWIN6 NUMBER. REVISION LETTER AND MANUFACTURERS SYMBOL PER NO 100201V. 

2. INSPECTION AND ACCEPTANCE 

A. DIMENSIONS: AS SHOWN ON DRAWING. 

R. CLEANLINESS: CONTANINANT PARTICLES SHALL NOT EXCEED ISO MICRONS IN SIZE WHEN TESTED 

PER (JiaX^J) 

C, PRESSURE TEST: ASSEMBLY MUST NOT DEFORM MIEN INTERNALLY PRESSURIZED TO 90 PS 10 WITH 
DISTILLED WATER. 

0. LEAK TEST: MAXIMUN LEAK RATE 5 X 1(T* STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
TO 77.5 t .5 PSIG (PERFORMED AFTER PRESSURE TEST). 

3. DESIGN REQUIREMENTS 

A. MATERIAL: ,, 

1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .00G/.008 WALL THICKNESS) 

2. BRAID: CRES CLASS 321 COND A PER QQ-S-763 

3. END FITTINGS: CRES CLASS 321 COND A PER QQ-S-703 

B. FINISH: PASSIVATE PER MIL-F-14072 FIN E-300 


4 . SPECIAL INSTRUCTIONS AND INFORMATION 

A. MACHINING: 

1. REMOVE BURRS AND BREAK SHARP EDGES .00S/.015. 

2. MACHINE SURFACES ^ FINISH 

B. WELDING: INERT WELD PER MIL-W-8G11. 

C. THREADS MUST CONFORM TO MIL-S-7742. 



LIST OF PARTS AMO MATERIALS 


HOSE FLEXIBLE 
WELDING ASSY 

OPTICS BASE TO LMU 


SEE NOTE 3 A 


CCMTOI 


1001468 
























3 





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REVISIONS T~Z>/e/$ 0?<3O 

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V£+Us #*\ 


ITDRR 11042. 


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THESE SURFACES SHALL BE 
FREE FROM LONGITUDINAL 
AND SPIRAL TOOL MARKS 


REQUIREMENTS: 

1. GENERAL 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. 

C. 


D. 


SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND1015404. CLASS 3. 
ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

1. PREVENT CONTAMINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

IDENTIFY USING DRAWING NUMBER. REVISION LETTER AND MANUFACTURERS SYMBOL PER NO 1002019. 


SPECIAL INSTRUCTIONS AND INFORMATION 
A. MACHINING: 

1. REMOVE BURRS AND BREAK SHARP EDGES .005/.015. 

2. MACHINE SURFACES ^ FINISH 


WELDING: INERT WELD PER MIL-W-8611. 
THREADS MUST CONFORM TO MIL-S-7742. 


INSPECTION AND ACCEPTANCE 
A. DIMENSIONS: AS SHOWN ON DRAWING. 

CLEANLINESS REQUIREMENTS PER ND 1002223. 


PRESSURE TEST: ASSEMBLY MUST NOT PERMANENTLY DEFORM WHEN INTERNALLY PRESSURIZED TO 90 PS IG WITH 
DISTILLED WATER. 

LEAK TEST: MAXIMUM LEAK RATE 5 X 10^ STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
TO 77 *4 PSIG (PERFORMED AFTER PRESSURE TEST). 

DESIGN REQUIREMENTS 
A. MATERIAL: 

1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .006/.008 WALL THICKNESS) 


B. 

C. 


2. BRAID: CRES CLASS 321 COND A PER QQ-S-7G3 

3. END FITTINGS: CRES CLASS 321 COND A PER QQ-S-7G3 
FINISH: PASSIVATE PER MJL-F-14072 FIN E-300 


CONFIGURATION 

1. FLEXIBLE HOSE SHALL BE CAPABLE OF BENDING TO A 1* INSIDE RADIUS WITHOUT DAMAGE OR PERMANENT SET. 







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LIST OF PARTS AND MATERIALS 


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SEE NOTE 4 B 



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45* i 5* 

5 PLACES 


.GBO uc< 
.<£>70 


-THESE SURFACES SMALL BE 
FREE FROM LONGITUDINAL 
AND SPIRAL TOOL MARKS 


REQUIREMENTS: 


GENERAL 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND1015404. CLASS 3. 

C. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

|. PREVENT CONTAMINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENDING OF THE NOSE TO A RADIUS OF LESS THAN 20 INCHES. 

». IDENTIFY USING DRAWING NUMBER. REVISION LETTER AMD MANUFACTURERS SYMBOL PER NO 1002019. 

INSPECTION AND ACCEPTANCE 

A. DIMENSIONS: AS SHOWN ON DRAWING. 

B. CLEANLINESS. REQUIREMENTS PER ND 1002223. 

C. PRESSURE TEST: ASSEMBLY MUST NOT PERMANENTLY DEFORM WHEN INTERNALLY PRESSURIZED TO 90 PSIG WITH 
DISTILLED WATER. 

D LEAK TEST: MAXIMUM LEAK RATE 5 X 10"* STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
TO 77 +4 PSIG (PERFORMED AFTER PRESSURE TEST). 

DESIGN REQUIREMENTS 
A. MATERIAL: 

1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .010/.012 WALL THICKNESS) 


SPECIAL INSTRUCTIONS AND INFORMATION 


1. REMOVE BURRS AND BREAK SHARP EDGES .005/.015. 

2. MACHINE SURFACES ^ FINISH 
WELDING: INERT WELD PER MIL-W-8611. 

THREADS MUST CONFORM TO MIL-S-7742. 


2. BRAID: CRES CLASS 321 COND A PER QQ-S-7G3 

3. END FITTINGS: CRES CLASS 321 COND A PER QQ-S-7G3 
FINISH: PASSIVATE PER HI L-F-14072 FIN E-300 

CONFIGURATION 

1. FLEXIBLE HOSE SHALL BE CAPABLE OF BENOING TO A 1- INSIDE RADIUS WITHOUT AFFECTING PERFORMANCE. 


LIST OF PARTS AMO MATERIALS 

HOSE FLEXIBLE 
WELDING A 55V 

OPTICS BASE TO LMU. 


SPACECRAFT CENTER 


SEE NOTE 3 A 


1001468 

SHEET » OF 


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- LEAVE SHARP - 


SEE NOTE 40 


-.003 MAX 


-.8125 -20 UNEF-3A 


MAJOR DIA J^44 


THIS SURFACE TO BE FREE OF RADIAL 

AND SPIRAL TOOL MARKS, ANNULAR GROOVES UP TO 32 MICRO - INCHES 


MEX 

ACROSS FLATS 


PITCH DIA * 77*57 


'*.182 MAX WILL BE PERMISSABLE 


MINOR DIA 7512-NOMINAL 


1. 6ENERAL 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY NIL-D-70327. 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND1015404, CLASS 3. 

C. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

1. PREVENT CONTAMINATION OF THE INTERNAL SURFACES. 

2. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

D. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL PER NO 1002019. 


SPECIAL INSTRUCTIONS AND INFORMATION 


1. REMOVE BURRS AND BREAK SHARP EDGES .005/.015. 

2. MACHINE SURFACES FINISH 


WELDING: INERT WELO PER HIL-W-8611. 


CONFIGURATION AND DIMENSIONS CONTROLLED 
BY SEATON WILSON MFC. CO. 

BURBANK, CALIFORNIA 


INSPECTION AND ACCEPTANCE 
A. DIMENSIONS: AS SHOW ON DRAWING. 


CLEANLINESS: CONTAMINANT PARTICLES SHALL NOT EXCEEO ISO MICRONS IN SIZE WHEN TESTED 

PER IXoXmJ) ■* 

PRESSURE TEST: ASSEMBLY MUST NOT DEFORM WHEN INTERNALLY PRESSURIZED TO 90 PSIG WITH 
01 STILLED WATER. 

LEAK TEST: MAXIMUM LEAK RATE 5 X 10 - * STD CC/SEC OF HELIUM WHEN INTERNALLY PRESSURIZED 
TO 77.5 t .5 PSIG (PERFORMED AFTER PRESSURE TEST). 


DESIGN REQUIREMENTS 


1. FLEXIBLE TUBING: CRES CLASS 321 (TRUE SEAMLESS .OOG/.OOB WALL THICKNESS) 
PER MIL-T-7880. 

2. BRAID: CRES CLASS 321 COND A PER QQ-S-7G3 

3. END FITTINGS: CRES CLASS 321 COND A PER QQ-S-7G3 


PASSIVATE PER MlL-F-14072 FIN E-300 


LIST OF PARTS ANO MATERIALS 


-rSr— HOSE FLEXIBLE "VZZSSSISf* 
WELDING AS5Y _— 

I *' ' III OPTICS BASE TO LMLU. - mmm > ~ 

LuwiT SPECIFICATION CONTROL DWG "WjSST 


> on I SEE NOTE 3 A A mt/pupm ml 


*1 I00I4GQ 


IIHCCT I OP I 




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Ji* 





ZONE SYM 


DESCRIPTION 


SKK LS&QOIS 

I MTf I APPROVAL ' 


TDRR MO-43 


7//4/&Y 


SEE NOTE 4 






IG.4Z REF- 


1. INTERPRET DRAM IN6 IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL 
PER HD100201V. 

3. ASSEMBLY SHALL BE PACKED AND SHIPPED IN a MANNER THAT MILL: 

A. PREVENT contamination of internal surfaces. 

B. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

C. PREVENT DAMAGE TO COUPLING HALF. 

.4. ATTACH TAG AT INDICATED AREA. TAG TO SAY "CAUTION - TEMPERATURE OF 
FITTING NOT TO EXCEED 500°F WHEN WELDING TO SPACE CRAFT" 

5. ASSEMBLE ITEM (T) TO ITEM (T) WITH 70 IN-LB i 7% TORQUE. 

6. LEAK TEST: WITH COUPLING HATED WITH NASA PART NO. 1000135. 

THE MAXIMUM LEAK RATE IS 5 X 10 -6 STD CC/SEC OF HELIUM WHEN INTERNALLY 
PRESSURIZED TO 77.5 ♦ .5 PSIG. 

7. CONFIGURATION AND DIMENSIONS CONTROLLED BY ICD MH01-01008-116. 


LUBRICANT, DOW CORNING NO. 55 

PACKING PREFORM _ 

COUPLING QUICK DISC. _ 

HOSE, FLEX. ASSY _ 

NOMENCLATURE 
OR DESCRIPTION 


IMIL-L-3434 


1000159-6 

1010797-1 

1001466 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MIT 

INSTRUMENTATION LAS 
CONTRACT 


LIST Of PARTS AND MATERIALS 

HOSE/ ASS V 
FLEXIBLE 

SPACECRAFT TO OPTICS BASE 


1015000 


COOE IDENT. 


INSTRUMENTATION 

LABORATORY 

Camwiiobb. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

IOOI469 


APPLICATION 


I SHEET | 


3 









































ZONE I SYM 


1 

REVISIONS T~DR£ Og6?>0 ~ 

DESCRIPTION I DATE I APPROVAL 



-SEE NOTE 1 D 


-SEE NOTE 4B 
REF 


1.19_.j 

,. 2 a—| 


COUPLING 




IG.48 

" 16.3 <3 



REQUIREMENTS 
1. GENERAL: 


A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL 
PER ND1002019. 

C. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

1. PREVENT CONTAMINATION OF INTERNAL SURFACES. 

2. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

3. PREVENT DAMAGE TO COUPLING HALF. 

D. ATTACH TAG AT INDICATED AREA. TAG TO SAY "CAUTION - TEMPERATURE OF 
FITTING NOT TO EXCEED 500°F WHEN WELDING TO SPACE CRAFT" 

INSPECTION AND ACCEPTANCE: 

A. ASSEMBLY SHALL MEET THE REQUIREMENTS OF PS1000135 EXCEPT PROOF AND 
BURST PRESSURE TESTS. 

B. COUPLING, QUICK DISCONNECT MUST MATE WITH NASA PART NO. 1000135. 

C. LEAK TEST: WITH COUPLING MATED WITH NASA PART NO. 1000135. 

THE MAXIMUM LEAK RATE IS 5 X 10“^ STD CC/SEC OF HELIUM WHEN INTERNALLY 
PRESSURIZED TO 77.5 i .5 PSIG. 


DESIGN REQUIREMENTS 
A. MATERIAL: 

1. HOSE ASSEMBLY; MAKE FROM NASA PART NO. 10014GG. 

2. COUPLING; SLEEVE AND BODY f CRES CLASS 300 SERIES 

PER QQ-S-763 
TRUNNION-STEEL 17-4 PH 

SNAP RING - CRES ARMCO PH 15-7MO OR AISI TYPE 420 


B. 

FINISH: 



1. COUPLING: 

PASSIVATE PER MIL-F-14072 FIN E-300 

C. 

LOCKING TYPE: 

PUSH TO CONNECT 



PULL TO DISCONNECT 


SPECIAL INSTRUCTIONS AND INFORMATION: 

A. CONFIGURATION AND DIMENSIONS OF INTERNAL COMPONENTS OF COUPLING 

AND ASSEMBLY OF COUPLING IS A PROPRIETORY PROCESS OF SEATON WILSON MFG. CO., BURBANK, CALIFORNIA. 

B. CONFIGURATION AND DIMENSIONS CONTROLLED BY I CD MHO I-01008-116. 


1014999 _ 

NEXT ASSY USED ON 

APPLICATION 


NOMENCLATURE 
OR DESCRIPTION 


i I wo. | 

LIST OF PARTS AND MATERIALS 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 

SEE NOTE 3A 


M I T 

INSTRUMENTATION LAG 
CONTRACT 

NAS 9153 rbATE " 


MIT/M. APPROVAL 


HOSE, ASS'y 
FLEXIBLE . 

SPACECRAFT TO OPTICS BASE 


UNIT WT. 


CODE (DENT. 


INSTRUMENTATION 

LABORATORY 

Gamewi po c. Mam, 

DRUM. WO. 

MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

IOOI469 

SHEET | OF I 






















8 


7 


6 



1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY NIL-D-70327. 
fe- IDENTIFY USING DRAWING NUMBER. REVISION LETTER AND MANUFACTURERS SYMBOL PER 
ND1002019. 

3. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

A. PREVENT CONTAMINATION OF INTERNAL SURFACES. 

B. PREVENT BENDING OF THE HOSE TO a RADIUS OF LESS THAN 20 INCHES. 

C. PREVENT DAMAGE TO C0UPLIN6 HALF. 

4. ATTACH TAG AT .INDICATED AREA. TAG TO SAY "CAUTION - TEMPERATURE OF FITTING 
NOT TO EXCEED 500*F WHEN WELDING TO SPACECRAFT 11 

5. ASSEMBLE ITEM Q> TO ITEM CD H,TM 70 ,IHJ * n T0RQUE * 

4. LEAK TEST: WITH COUPLING MATED WITH NASA PART NO. 1000135. 

THE MAXIMUM LEAK RATE IS 5 X 10‘* STD CC/SEC OF HELIUM WHEN 
INTERNALLY PRESSURIZED TO 77.5 ± .5 PSIG. 

7. CONFIGURATION AND DIMENSIONS CONTROLLED BY ICD MHOI>01008-114. 




















SEE NOTE 4 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY NIL-D-70327. 

2* IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL PER 
ND1002019. 

3. ASSEMBLY SHALL BE PACKED AND SHIPPEO IN A MANNER THAT WILL: 

A. PREVENT CONTAMINATION OF INTERNAL SURFACES. 

B. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

C. PREVENT DAMAGE TO COUPLING HALF. 

4. ATTACH TAG AT INDICATED AREA. TAG TO SAY -CAUTION - TEMPERATURE OF FITTING 
NOT TO EXCEED 500*F WHEN WELDING TO SPACE CRAFT- 

5. ASSEMBLE ITEM QT) TO ITEM WITH 70 IN-LB i 7* TORQUE. 

4. LEAK TEST: WITH COUPLING MATED WITH NASA PART NO. 1000135. 

THE MAXIMUM LEAK RATE IS 5 X 10“* STD CC/SEC OF HELIUM WHEN 
INTERNALLY PRESSURIZED TO 77.5 t .5 PSIG. 

7. CONFIGURATION AND DIMENSIONS CONTROLLED BY ICO MNOI-01008-114. 





























>¥»* 

•:twrr 


i m 


i 


-SEE NOTE A0 
REF 




SEE NOTE ID- 


REQUIREMENTS 

1. GENERAL: 

ft. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY NIL-D-70327. 

B. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL PER 
ND1002019. 

C. ASSEMBLY SHALL BE PACKED ANO SHIPPED IN A MANNER THAT WILL: 

1. PREVENT CONTAMINATION OF INTERNAL SURFACES. 

2. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

3. PREVENT DAMAGE TO COUPLING HALF. 

». ATTACH TAG AT INDICATED AREA. TAG TO SAY “CAUTION - TEMPERATURE OF FITTING 
NOT TO EXCEED 500*F WHEN WELDING TO SPACECRAFT - 

2. INSPECTION ANO ACCEPTANCE: 

ft. ASSEMBLY SHALL MEET THE REQUIREMENTS OF PS1000135 EXCEPT PROOF AND BURST 
PRESSURE TESTS. 

ft. COUPLING, QUICK DISCONNECT MUST MATE WITH NASA PART NO. 1000135. 

C. LEAK TEST: WITH COUPLING MATED WITH NASA PART NO. 1000135. 

THE MAXIMUM LEAK RATE IS 5 X 10“^ STD CC/SEC OF HELIUM WHEN 
INTERNALLY PRESSURIZED TO 77.5 t .5 PSIG. 


DESIGN REQUIREMENTS 

A. MATERIAL: 

1. HOSE ASSEMBLY; MAKE FROM NASA PART NO. 1001467. 

2. COUPLING; SLEEVE AND BODY - CRES CLASS 300 SERIES PER QQ-S-763 

TRUfflON- STE& 17-4PH 

SNAP RING - CRES ARMCO PHI5-7 NO OR AISI TYPE 420 

B. FINISH: 

1. COUPLING: PASSIVATE PER MlL-F-14072 FIN E-300 

C. LOCKING TYPE: PUSH TO CONNECT 

PULL TO DISCONNECT 

SPECIAL INSTRUCTIONS AND INFORMATION: 

ft. CONFIGURATION AND DIMENSIONS OF INTERNAL COMPONENTS OF COUPLING 
AND ASSEMBLY OF COUPLING IS A PROPRIETORY PROCESS OF 
SEATON WILSON MFG. CO. 

BURBANK, CALIFORNIA. 

B. CONFIGURATION AND DIMENSIONS CONTROLLED BY ICD MHOI-OIOOS-II6. 


NOMCNClATUftC 
on oncmmoN 


wurr on I 
loo nmw no. 


I T0ttW«O ON 


LIST OF PARTS AMO MATERIALS 

. HOSE, ASS'Y : 

FLEXIBLE 

I.M.U. TO SPACECRAFT 
SPECIFICATION CONTROL DWG 


SEE NOTE 3A 


MarntUMCNTATIOM 

LAffOftATOffY 


ffACCCAAFT COffCR 

idolTfo 






























1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. IDENTIFY USING DRAWING HUNGER. REVISION LETTER AND MANUFACTURERS SYMBOL 
PER ND1002019. 

}• ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

A. PREVENT CONTAMINATION OF INTERNAL SURFACES. 

B. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

C. PREVENT DAMAGE TO C0UPLIN6 HALF. 

4. ASSEMBLE ITEM (T) TO ITEM CD M,TM 70 ,IHJ 1 71 TWQUE ‘ 

5. LEAK TEST: WITH COUPLING MATED WITH NASA PART NO. 1000135. 

THE MAXIMUM LEAK RATE IS 5 X 10"^ STD CC/SEC OF HELIUM WHEN 
INTERNALLY PRESSURIZED TO 77.5 i .5 PSIG. 



AfR 

LUBRICANT .OOVN CORUING N0.S5 

. 

KUL-L- 4343 

.... .... . 

4 

\ 

PACKING . PREFORM 

IOOOI5VG 



3 

" l ' 

COUPLING QUICK -- 

I0X07B7- l 



2 


HO^E.PUty. 

I0014GS 

- . 

■ — . 

m 

«d 

NOMKNCUTUM 

OR OCSCMRTMM 

1 -fy 0 * 

1 MNDfYM NO. 


MATKMAL 

B 



LKT OF PARTS AMO MATERIALS 

_.HOSE, ASS'Y 

* FLEXIBLE 



, _ OPTICS BASE TO I MU 


TEST 

£-1 


WIT 


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M8A araerr? ■». 

1001471 


i or l 


A 


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1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. IDENTIFY USING DRAWING NUMBER, REVISION LETTER AND MANUFACTURERS SYMBOL 
PER ND1002019. 

}• ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

PREVENT CONTAMINATION OF INTERNAL SURFACES. 

|. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

C. PREVENT DAMAGE TO COUPLING HALF. 

4. ASSEMBLE ITEM <J) TO ITEM CD WITH 70 IN-LB ± 7* TORQUE. 

5. LEAK TEST: WITH COUPLING MATEO WITH NASA PART NO. 1000135. 

THE MAXIMUM LEAK RATE IS 5 X 10~ b STD CC/SEC OF HELIUM WHEN 

INTERNALLY PRESSURIZED TO 77+4 PSIG. 

-0 

6. CLEANLINESS REQUIREMENTS PER ND1002223. 

























REQUIREMENTS 

1. GENERAL: 

A. INTERPRET DRAWIN6 IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 
I. IDENTIFY USING DRAWING NUMBER. REVISION LETTER AND MANUFACTURERS SYMBOL 

PER ND1002019. 

C. ASSEMBLY SHALL BE PACKED AND SHIPPED IN A MANNER THAT WILL: 

1. PREVENT CONTAMINATION OF INTERNAL SURFACES. 

2. PREVENT BENDING OF THE HOSE TO A RADIUS OF LESS THAN 20 INCHES. 

3. PREVENT DAMAGE TO COUPLING HALF. 

2. INSPECTION AND ACCEPTANCE: 

ft. ^ASSEMBLY SHALL MEET THE REQUIREMENTS OF PS1000135 EXCEPT PROOF AND BURST 

Pressure tests. 

B. COUPLING. QUICK DISCONNECT MUST MATE WITH NASA PART NO. 1000135. 

C. LEAK TEST: WITH COUPLING MATED WITH NASA PART NO. 1000135. 

THE MAXIMUM LEAK RATE IS 5 X 10~* STD CC/SEC OF HELIUM WHEN 
INTERNALLY PRESSURIZED TO 77.5 1 .5 PSIG. 


3. DESIGN REQUIREMENTS 

A. MATERIAL: 

1. HOSE ASSEMBLY; MAKE FROM NASA PART NO. 1001461. 

2. COUPLING; SLEEVE ANO BODY - CRES CLASS 300 SERIES PER QQ-S-763 

TRUNNION - STEEL 17-4PM 

SNAP RING- CRES ARMCO PHI5-7 MO OR AlSI TYPE 420 

B. FINISH: 

1. COUPLING: PASSIVATE PER MIL-F-14072 FIN E-300. 

c. Cocking type: push to connect 

PULL TO DISCONNECT 

R. SPECIAL INSTRUCTIONS AND INFORMATION 

A. CONFIGURATION AND DIMENSIONS OF INTERNAL COMPONENTS OF COUPLING 
AND ASSEMBLY OF COUPLING IS A PROPRIETORY PROCESS OF 

SEATON WILSON MFG. CO. 

BURBANK. CALIFORNIA 














GGh 


mire harness a 


■100147* 



GOH 


MIRE HARNESS A 


1001474 


_*_ 

PENNANT 

NOTE 

ITEM 

OTY 

LIST OF MATERIALS 

PART NO DESCRIPTION 







1 

1 

1010416- 

1 

WIRE. MIL-W-16878E28. 28AWG* 
4.75 IN* TOT* LG 

BLK* 

20 FT 




2 

1 

1010416- 

3 

WIRE* M1L-W-16878E28* 28AWG* 
11*37 IN* TOT* LG 

RED* 

11 FT 




3 

1 

1010416- 

9 

WIRE* MIL-W—16878E28* 28AMG* 
TOT* LG 

GY* 

1 FT 10*16 

IN. 



4 

1 

1010416- 

8 

WIRE* MIL-W-16878E28* 28AWG* 
TOT. LG 

VIO* 

7 FT 3.25 

IN. 



3 

1 

1010416- 

7 

WIRE* MIL-W-16878E28* 28AMG* 
TOT. LG 

BLU* 

3 FT 6*50 

IN. 



6 

1 

1010416- 

4 

WIRE* MIL-W-16878E28* 28AWG* 
10.25 IN. TOT. LG 

ORN* 

6 FT 




7 

1 

1010416- 

6 

WIRE* MIL-W-16878E28• 28AWG* 
7*38 IN. TOT. LG 

GRN* 

29 FT 




8 

1 

1010416- 

3 

WIRE* MIL-W-16878E28* 28AWG* 
4*25 IN* TOT. LG 

YEL* 

22 FT 




9 

1 

1010416- 

10 

WIRE* MIL-W-16878E28* 28AWG* 
11.88 IN. TOT. LG 

WHT • 

4 FT 




10 

1 

1010416- 

2 

WIRE* MIL-W—16878E28* 28AWG* 
TOT. LG 

BRN* 

2 FT 6*75 

IN. 



11 

1 

1010778- 

1 

WIRE* SHIELDED* 
TOT. LG 

28AWG* 1 COND 9 FT 6*9 IN* 




12 

1 

10UQJ78- 

2 

WIRE* SHIELOEO* 
TOT. LG 

28AWG* 2 COND 10 

FT 7.5 IN. 









MANNED 

SPACECRAFT 

CENTER 

HOUSTON, TtXAS 

SIZE 

A 

1001474 







SCALE-NONE 

REV LTR A 


J SHEET A OM ?°] 





\ ' G0H MIRE HARNESS A A 1001474 

_ _ ^ 

i PtNNAM GENERAL NOTES 

NOTE 

12 LENGTH* IN CONOuCTOR CHART ARE FOR REFERENCE ONLY 

DETAILS B AND C ON CONFIGUKATION SHEET FOR METHODS OF 
TERMINATING SHIELDS 

14 IDENTIFY USING DRAMING NO.* REVISION LETTER AND MANUFACTURERS 

SYMBOL PER ND1002019 AND SERIALIZE PER ND1002C23* 


MANNED 

SPACECRAFT 

CENTER 

HOUSTON. TEXAS 


SIZE 

A 


A 


1001474 


, u v r • ' 


-fs 



SCALE-NONE I REV LTR 


SHEET 


3 OF 2 































GOH 


WIRE HARNESS A 


A 


1001474 


pennant list of materials 


ITEM QTY 

13 1 

PART NO 

1010776- 

3 

DESCRIPTION 

WIRE* SHIELDED. 28AWG* 3 COND 
TOT. LG 

1 FT 4*5 IN* 

14 

3 

1000121 


CONNECTOR* RECEPTACLE 


1* 

3 

1000122 


CONNECTOR* RECEPTACLE 


16 

3 

1010318- 

1 

CONNECTOR* PLUG 


17 

1 

1010472- 

1 

CONNECTOR* PLUG 


18 

2 

1000120 


CONNECTOR* PLUG 


19 

1 

1001474- 

11 

SHIELD-WIRE* QQ-B-575* 17/64 
6.62 IN. LG 

I D 36AWG)* 

20 

1 

1001474- 

12 

SHIELD-WIRE* QO-B-575. (7/64 
9.00 IN. LG 

I D 36AWGI* 

21 

2 

1001474- 

13 

SHIELD-WIRE* QO-B-575* 17/64 
4.62 IN. LG 

1 D 36AWGJ• 

22 

1 

1001474- 

14 

SHIELD-WIRE* QO-B-575* 17/64 
18.50 IN. LG 

I D 36AWGI* 

23 

1 

1001474- 

15 

SHIELD-WIRE* QQ-B-575* 17/64 
4.12 IN. LG 

I D 36AWG)* 

24 

AR 

1010490- 

983 

SLEEVING-HEAT SHRINK. WHT* 55 IN. TOT. LG 

25 

7 

1010490- 

114 

SLEEVING-HEAT SHRINK* 


26 

7 

1010490- 

058 

SLEEVING-HEAT SHRINK* 


27 

42 

1010490-084 

SLEEVING-HEAT SHRINK* 



MANNED 

SPACECRAFT 

CENTER 

HOUSTON, TEXAS 

SIZE 

A 


SCALE - NONE 

REV LTR 

A 


1001474 


SHEET 


GOH 


WIRE HARNESS A 


A 1001474 



•IE 

■1 


S 





^B 


B 


I 

■ 

K3 

e 



m 

1 

■ 

fl 



MB 


P*M 


|i 


11 

tj| 

fl 

B 


|l 

1 


m 


la1 

I 


m 

■ 


m 



11 


■ 

BE 



■ 

E 

m 

E 

El 



e; 

III 


El 




B 

QUI 


is 

g 

1 

El 

■ 



Bl 



E 

El 

E 

SI 



e: 

III 


El 




E 

bbi 


is 


1 

El 

■ 



Bl 

bbbi 


E 

■ 

E 

I 



Si 

III 


El 




S 

BIBi 


Ei 


1 

El 

■ 



Bl 

■Bl 


E 

■ 

E 

El 



Si 

III 


El 




B 

son 


Ei 



El 

■ 



Bl 

B— 


E 

E 

E 

S 



Si 

ill 


El 




E 

QBB 


Ei 



B! 

■ 



Bl 

Bl 


D 

E 

E 

1 



Si 

I 


B 




E 

obu 


Ei 



Bl 

■ 



El 

m 


E 

E 

E 

1 



Si 

I 


■ 




B 

B]IB 


SI 



fl 

fl 



BBS 

BB 


E 

E 

E 

z 



Si 

;i 


fl 




E 



SI 



fl 

fl 



B! 

bbh 


E 

B 

B 

1 



1 

i 


■ 




fl 



Si 



fl 

fl 



Bl 

m 


E 

B 

E 

I 



i 

;■ 


■ 




B 

QBBI 


Si 



E 

fl 



Bl 

bbb 


E 


B 

1 



■ 



■ 




B 

QBH 


Si 



B 

E 



Bl 

■bbi 


E 


■ 

1 



IB 

« 


fl 




B 

Bin 


Si 



E 

■ 



Bl 

BH 


E 


IB 

I 



■ 

a 


E 




E 

SQH 


ISi 



B 

B 



Bl 

Bl 


E 


E 

I 



ISi 

» 


E 




fl 

SQH 


ISi 



B 

■ 



Bl 

BiHI 


E 


E 

I 



ISi 

a 


B 




B 

BBB 


in 



B 

■ 



B! 

■bbi 


n 


E 

I 

bbi 


ISi 

a 


■ 




B 

am 


ISi 



■ 

■ 



Bl 

Bl 


E 


E 

I 

BH 


IS! 

!■ 


■ 




B 

mi 


IS 



B 

■ 



B 

■BHi 


E 


IE 

I 

I9B9H 


IS 

i 


B 




B 

m 


IS 



B 

■ 



IB 

BIHI 


MANNED 


THE STD CONDUCTOR TERMINATION FIOURIS ARE PER 
DIMENSIONS ARE M INCHES AND TWO PLACE DECIMALS. 


SPACECRAFT 

CENTER A 

HOUSTON, THAI 


SCALE • NONE REV LTR 


A 


1001474 


SHEET 7 OF 


GOH 


MIRE HARNESS A 


1001474 


PENNANT 



list of materials 


NOTE 

ITEM 

0TV 

PART NO 

DESCRIPTION 



28 

12 

1000243- ? 

I FERRULE* INNER 



29 



DELETED 11000242- 5) 



30 

130 

1006776- 18 INSULATION* SLEEVING .31 

LG 


31 

49 

1006776- 16 INSULATION* SLEEVING .31 

LG 


32 

• 

1010717- 1 

1 TERMINAL LUG 



33 

1 

1000267 

BRACKET 



34 

1 

1000226 

BRACKET 



35 

1 

1000149 

BRACKET 



36 

AR 

QQ-S-571 

SOLDER ISN60WARP2) 



37 

AR 

MIL-T-713 

TAPE* NYLON* WAXED* TYPE 

P* CLASS 2* BLACK 



MANNED 

SPACECRAFT 

CENTER 
HOUSTON, THAI 

SIZE 

A 

1001474 


SCALE-NONE j 

REV LTR 

A 

| SHEET 6 OF 


E 


Wire harness a 



SCALE-NONE 



























































GOH 


WIRE HARNESS A 


1001474 


r— 

i 

ONDUCT 

INDIVIDUAL It 


—| 

FROM 



MOTH 

> 

CUT WIM OR SHIHO 

strip win or jackst ii> 



TRRMMU 

SKC 


CUT WIM Ot SHIELD 


> 

■ 

■ 

uTfSm9m 

a 


il> 

NO. 

STOP WIM Ot JACKET 

> 

IP 




[£= 

S9 

19 

_i 



It> 

i 

IKM 

NO. 1 


CIRCUIT POINT 

jp 



jfl 

A 

22 G 

7 

5 

00 

J19-L 


icy 



30 




23 

J20-L 


10 Y 







24 


A 

22Y 

8 

5 

00 

J19-D 


107 



30 




23 

J20-D 


10Y 







24 


A 

230 

6 

5 

00 

J19-C 


ICY 







23 

J20-C 


10Y 



31 




24 


A 

23V 

4 

5 

oc 

J19-F 


107 







23 

J20-F 


10Y 



31 




24 


A 

24K 

1 

17 

06 

J20-B* 


ICY 



30 




24 

J14-U 


10Y 



30 




3 


A 

24N 

10 

17 

06 

J20-D* 


ICY 



30 




24 

J14-V 


10Y 



B 




3 


A 

24M 

9 

17 

0C 

J20-Y 


ICY 



3C 




24 

J14-T 


10Y 



30 




■1 


A 

27A 




J30- 2 









51 

SHLD A27 


25! 







IBI 


A 

27B 

1 

4 

81 

SHLD A27 


25! 







24 

J2C-P 


10Y 



30 




24 


A 

27K 




J30- 1 









51 

J20-J 


10Y 



30 




24 


A 

27R 




J30- 3 









51 

J20-N 


10 Y 

f 


30 




2 * 


A 

27V 




J30- 8 





28 




51 

J20-M 


10 ' 

f 


21 




24 


A 

28 

11 

12 

44 


2 

75 









1 

CO 









A 

28A 

1 

2 

5C 

SHLD A28 


13 



27 





•39 


13 

1 


27 




24 


A 

28G 




J20-E 


10 

Y 






24 

*3 


13 

Y 






38 


A 

29 

11 

7 

5 C 


2 

75 









1 

50 









A 

29B 

1 

1 

5C 

E39 


13 

Y 


2 ! 

2t 



34 

ASHLD A29 


13 

V 


27 






A 

29G 

cr 


J20-F 


1C 

Y 






24 

A16“ 2 

rs 

13 

y 

— 






IEI 



>THK STD CONDUCTOR TERMINATION FIGURES ARE FER 
> DIMENSIONS ARE IN INCHES ANO TWO FIACS DECIMALS. 


MANNtO 

SFACECRAFT 

CENTER 


1001474 


SCALE-NONK 


I SHEET 9 OF 2 0 



GOH 


MlRE HARNESS A 


1661474 


Jr 


u 


■1 




■ 


ll 


■■1 


n — nTT1TT) 

L 

| CUT WIM OC SHIHD 




TERMINATION 




ng 

BE! 

■i 


■i 



IPtC. 


r 

1 ST1IP WIM OC JACXVT 

T 

Tl!> 



SPCC 

NO. 


IE331I 

□ 

KSm\ 


isi 

MM 

rr«M no. | 


L__ 

IHB23SEZ3HI 

2 > 1 . 


rruH no. | 




3 

□ 

Bl 

E 

El 


i 

El 



Bl 




in 

bh 

i 

SI 



□ 

□ 





3 

30A 

■1 

B 

Z 


1 

IS 



B 





SHHBI 


s: 



Bl 

E 



24 : 


F 

30G 

B 

B 

1 



Ei 



B 




24 

3BEBB 


i; 



Bl 




32 


B 

KB 

Bl 

B 

1 



E 



B 





BHHI 

i 

1 

31 



B 






a 

310 

■ 

B 

I 



3 



B 





E35 


3! 



B 




24 


F 

31G 

B 

B 

1 

J20-C 


3 



B 




24 

R2 


b: 



B 




65 


D 

33 

B 

B 

I 

sggm 


3 



B 




1 

P15-W 


Bi 



B 




5C 


B 

BE 

B 

B 

1 



3 



B 




1 

J14-H 


BE 



B 




3 


D 

BE 

B 

B 


P17-B* 


3 



B 




1 

J14-J 


Ei 



B 




3 


D 

KB 

B 

B 

I 

P17-Y 



r 


* 




1 

J14-K 


Bi 



B 




3 


D 

ED 

B 

B 


P17-2 


3 



B 




1 

P17-T 


Bi 



B 




1 


B 

EB 

B 

B 

3 

P17-W 


5 



E 




1 

P16-C* 


Ei 



E 




2 


B 

IB 

E 

B 

3 

P17-V 


Si 



B 




1 

P15-V 


Bi 



B 




50 


B 

IQS 

IB 

B 

3 

mm 


Bi 



B 




1 

P15-S 


Ei 



B 




50 


B 

BE 

IB 

B 

3 

3BH1 


I 



B 




1 

P15-U 


Bi 



B 




50 


B 

BE 

IB 

B 

3 

^ 17-V 


IBi 



■ 




1 

P16-V 


IBi 



B 




2 


B 

EE 

IB 

B 

13 

'9WBBBHI 


I 



B 




1 

P16-N 


IBi 



B 




2 


B 


B 

IB 

3 

mmmmm 


131 



■ 




1 

P16-U 


Bi 



B 




2 


n 

> THE STD CONDUCTOR TERMINATION FIGURES ARE FER 


MANNtO 

SFACECRAFT 

CENTER 

HOUSTON, TtXAS 

s 

IZE 

A 

1001474 

l5 











SCALE-NONE 

[ REV LTR 


m 

■■ 

j SHEET 10 OF 20| 


GOH nIRE HARNESS A A 1001474 


1_CONDUCT 

| MOIVIOUAI U 

OR 





NOTH 

CUT WWf OR SHIHD 

> 

THMINATION 

| CUT WIM OR SHIHD 

t> 

THMINATION 



ITtM 

£> 

STRIP WIRt OR JACKIT 1 


SPK. 

a> 

NO. 

i ■srr! | i ,, i i !i."i*rT:aBi 

Hit 

spk rt> 

NO. 

NUMMC 

NO. 

CIRCUIT POINT 


iT 

ITRM NO. 

CIRCUIT POINT 


Hum 

IT1M NO. 


A 47L 




9 17-B 


10Y 







1 

P16-B 


i: 



B 




2 


A 48 

12 

24 

OC 


1 

00 










SI 



B 






A 48A 

1 

1 

5C 

SHLD A48 


1 3 Y 



27 




■1 

E34 


Ei 



B 




1 / 


A 48K 




P17-F 


ICY 



31 




1 

P15-F 


Si 



B 




50 


A 48L 




P17-C 


ICY 



31 




1 

P15-C 


Bi 



B 




5C 


A 49 

12 

9 

62 



OC 










Bl 



fl 






A 490 

1 

2 

5C 

E35 


13Y 



25 

B 



2 / 

iSQBSH 


Ei 



B 






A 49K 




P17-F 


1C 



27 




1 



Bi 



B 




2 


A 491 




P17-C 


ICY 







1 

P16-C 


Bi 



B 




2 


A 50E 

3 

9 

12 

P16-Y 


ICY 



3C 




2 

J14-S 

1 

Bi 



B 




3 


A 50L 

K 

9 

12 

P16-D* 


ICY 



3C 




2 

J14-P 

1 

Bi 



B 




3 


A 50V 

4 

9 

12 

P16-B* 


10Y 



3C 




2 

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1 

Si 



B 




3 


A 52 

2 

9 

OC 

P16-2 


1C' 



3C 




2 

P16-T 

1 

Si 



B 




2 


A 54 

6 

8 

87 

P16-W 


1C' 



30 




2 

J13-B 


Si 



B 




54 


A 55E 

3 

8 

87 

P16-V 

“1 

10 







2 

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1 

Si 



B 



1 

54 


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1 

8 

87 

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10 



31 




2 

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B 



1 

54 


A 55M 

9 

8 

87 

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10 

Y 






2 

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1 

IS! 



B 



I 

54 


A 56A 

1 

1 

50 

SHLD A56 


25 

Y 







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1 

IBi 



IB 

IB 


II 

67 

t 


STD CON 

DU 

CTOR TERMINATION FIGURES ARE FER 


MANNtO 

SFACECRAFT 

CENTER 

HOUSTON, TtXAS 

s 

IZE 

A 

1001474 

r 

SCALE-NONE 

REV LTR A j SHEET 12 OF 20| 





































































































































































































































































































































































6 Oh 


IRE HARNESS A 


1001474 


CONDUCTORS TO St TWISTED HER TMt wlRE IWlbTING CHART. 

SuFFlX LETTER^ ON CONDUCTOR NuMBlkS INDICATE THE FOLLOWING 
A - SHIELD GROUND ON FrOV. END N - bROWN 

B - SHIELD GROUND ON TO END 0 “ OkANGE 

C - WHT/ORN R * RED 

D - WHT/SLR/BRN S - WHT/BLK 

E - GRAY T " WHT/BRN 

F - WHT/5LK/RED u - «»HT/GY 

G - GREEN v “ VIOLET 

H - WHT/BLJ W " WHlTE , rt 

J - WHT/^ED x " WHT/V10 

* - slack l “ YE t•:?" 

L - BLUE P * WHT/GRN 

M - WHT/YEL 

Y OR N IN TINNED COLUMN INDICATES YES OR NO. 

DIMENSIONS ARE IN INCHES AND TWO PLACE DECIMALS 
SOLDER PER MIL-STD-440 USING ITEM 36 
LACE CABLE USING ITEM 37 

SPARE LEADS ON CONNECTORS J21* 028* 029* AND 030 TO BE CUT TO 
10 INCHES AND LACED INTO HARNESS 

CONDUCTORS WITH THE SAME NUMBER ARE TWISTED TOGETHER 
INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

MARX CHARACTERS .10- .14 HIGH COLOR BLACK PER ND 1002019 AT 
LOCATIONS SHOWN 

LENGTHS SPECIFIED FOR CONDUCTORS ARE for AFTER TWISTING 



GOH 


WIRE HARNESS A 


1001474 


_ 

GENERAL NOT Ei 

LENGTHS IN CONDUCTOR CHART ARE FOR REFERENCE ONLY 

SEE DETAILS B AND C ON CONFIGURATION SHEET FOR METHODS OF 

TERMINATING SHIELDS 

IDENTIFY USING DRAWING NO.* REVISION LETTER AND MANUFACTURERS 
SYMBOL PER ND1002C19 AND SERIALIZE PER ND1002023. 



MANNEO 

SPACECRAFT 

CENTER 

HOUSTON, TEXAS 

SIZE 

A 

1001474 

SCALE- NONE 

REV 1 

_ TR A | SHEET 3 OF 2 0 


E 


pennant 

NOTE 

12 

13 

14 


GOH 


WIRE HARNESS A 


A 


pennant 

NOTE 


LIST OF MATERIALS 


TEM i 

□TV 

PART NO 

DESCRIPTION 


13 

1 

1010778- 3 

WIRE* SHIELDED* 28AWG* 3 COND 
TOT. LG 

1 FT 4.5 IN. 

14 

3 

1000121 

CONNECTOR* RECEPTACLE 


1& 

3 

1000122 

CONNECTOR* RECEPTACLE 


16 

3 

1010318- 1 

CONNECTOR* PLUG 


17 

1 

1010472- 1 

CONNECTOR* PLUG 


18 

2 

1000120 

CONNECTOR* PLUG 


19 

1 

1001474- 11 

SHIELD-WIRE* QG-B-575* 17/64 
6*62 IN* LG 

I D 36AWGI* 

20 

1 

1001474- 12 

SHIELD-WIRE* QQ-B-575* (7/64 
9.00 IN. LG 

I D 36AWGI• 

21 

2 

1001474- 13 

SHIELD-WIRE* QQ-B-575* (7/64 
4.62 IN. LG 

1 D 36AWGJ• 

22 

1 

1001474- 14 

SHIELD-WIRE* QQ-B-575 * (7/64 
18.50 IN. LG 

I D 36AWGI* 

23 

1 

1001474- 15 

SHIELD-WIRE* QO-B-575• (7/64 
4.12 IN. LG 

I D 36AWG)* 

24 

AR 

1010490-983 

SLEEVING-HEAT SHRINK* WHT* 55 

IN. TOT. LG 

25 

7 

1010490-114 

SLEEVING-HEAT SHRINK* 


26 

7 

1010490-058 

SLEEVING-MEAT SHRINK* 


27 

42 

1010490-084 

SLEEVING-HEAT SHRINK* 



MANNED 


SIZE 


SPACECRAFT 

CENTER A 

HOUSTON, TEXAS 


SCALE-NONE j REV LTR 


A 


1001474 


1001474 


| SHEET 5 OF 2 














WIRE HARNESS A 


1001474 


PENNANT 

NOTE 


ITEM OTV 


list of materials 

PART NO DESCRIPTION 


28 

12 

1000243- 

5 

FERRULE* INNER 

29 




DELETED (1000242- 5) 

30 

130 

1005776- 

18 

INSULATION* SLEEVING .31 LG 

31 

49 

1006776- 

16 

INSULATION* SLEEVING .31 LG 

32 

8 

1010717- 

1 

TERMINAL LUG 

33 

1 

1000267 


bracket 

34 

1 

1000226 


BRACKET 

35 

1 

1000149 


BRACKET 

36 

AR 

QQ-S-571 


SOLDER (SN60WARP2) 

37 

AR 

MIL-T-713 

TAPE. NYLON* WAXED* TY»E P* 


MANNEO 

SPACECRAFT 
CENTER 
HOUSTON, TEXAS 


SCALE-NONE 


SIZE 

A 


1001474 


a IRE HARNESS A 


U 31474 



1001474 





































HIRE HARNE’>b A 


It5l474 





1001474 



1001474 



















































































GOH 


WIRE HARNESS A 


1001*74 



|>>THI STD CONDUCTOR TERMINATION FIGURES ARE FER 
|V> DIMENSIONS ARE IN INCHES AND TWO PIACE DECIMALS. 




SHEET 17 OF 






































1 

































































































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— ^ ^ 




1001474 


•A 


PfcAAAAP , ^,I4T Of MATERIALS 

•^A0T6 ^HEA OfV RA8T A<^ r ♦. OfSCRlWtON A* % ■ 

,;. 1 1 * -iOlOAU- .1 ,-WlHE, MlL-A-l687Bta«. 28AM6* BUC. 20 FT > ' 

* - ^ ^ A. , V , ,IA. TOT. LO ft .. 

■*•7 ■'* * ». . .'4" ■.• ' ; , , , ' ‘ • * » 4 * 

. I 2 ^*. ,1010414- J WfRf. H|L«W-14878EZ8. 2BAWG* RED* U FT " t „ 

* *' • ... ■ *, 11.17 IA. TOT ».LG 

,*■' .» ' - ■,;# ■*' 

i 'k i* 1 - t . 101C4*4» 9 AlPf. A1L-A-16878E28. 28A«G. 07. 4 FT 10.14 

-*w- J; ^ ^ . % - , tot. ls ■ ** 

#k . ; 4 Av 1010416- 4 «IRE» MIL-IK16d76E28. 26A4G* V10. 7 FT 3.24 

U< H^“ ' •> , TOT. LO 

W"* \ . 9 7 i ^ 1010414- " 7 A!4E* AiL-A-14874£26• 28AMG* BLGt 5 Ft 4.^) 

' •> % .% • ' - TOT. LG 

, . ■ ^ „ m . - e- ■ 

*■; •.-• * ^r v.-V -.1 U010414- 4 RjREt AJL-«-14478E24» ‘fcOAAG* GH\, 4 FT 

f * . ' . V . 10.26 14. TOT. LG 

. m* * * - - ‘ 

,* .. 7 ^ * 1010414- 4 WIRE* HIL-R-1G676E24, 28AWG* GR*. 29 FT 

i * » . ,. 7*38 IN.. TOT. LG 


1/S- 

IN. 


.. ■ v' 

AG .•_ 


U - ‘ 


*.8 *1010414- ,4 w! 7E* MIL-W-16878E26. 2d*WG* tEL* 22 FT , 

*-* *' ; ; # 4.25 I A. TOT. LG . * 

. *r . ’ v •* 

.t-9 1 ? 10UH116- 10 TURE, MJL-W-16676628. 28AWG* WHT. 4 FT 

V*>* ^ 11.88 IN. TOT. LG ^ 

10 4 /1010414- 2 WIRE, K1L-W-14878I.28. 28AWG* BRN. 2 FT G.7> IN.* 

- •! . TOT. LG 

A m _ • *- 

* il > 1010778- 1 WIRE* SHIELOEO* 28AWu. 1 10 AU 9 Ff 4.9 IN. ** 

* r * TOT. LG # 

1? /,i * 1010778- 2 WIRE. SHIELOEO. 26A»G* 2 CO\G 10 FT 7.9' IN. 

^ - 1 ‘ • *•/ TCT. LG -V ^ 




H 

% k- m 


m*mto 

SPACECRAFT 
CENTER 
NOUJTOM. nuu 


size 

A 


* S V: 








I 










































jasmin 



















































































































































































































































































































































CONDUCTORS TO BE TWISTED PER THt mIRL IwIsTINO CHART* 

SoFFlX LETTERS ON CONDUCTOR NuMbEkS iNoICATt THt FOLLOWING 
A - SHIELD GROUND ON FkOM END N - BROWN 

B - SHIELD GROUND ON TO END 0 - ORANGE 

C - WHT/ORN R - RED 

D - WHT/BLK/BRN S - whT/BLK 

E - GRAY T - WHT/BRN 

F - WHT/BLK/RED U - WHT/GY 

G - GREEN V - VIOLET 

H - WHT/BLU W - WHITE 

J - wHT/fttD X - WHT/VIO 

K - BLACK, Y - YELLOW 

L - BLUE P - WHT/GRN 

M - WHT/YEL 

Y OR N IN TINNED COLUMN INDICATES YES OR NO* 

DIMENSIONS ARE IN INCHES AND TWO PLACE DECIMALS 
SOLDER PER MIL-STD-440 USING ITEM 36 
LACE CABLE USING ITEM 37 

SPARE LEADS ON CONNECTORS J21* J28. 029* AND 030 TO BE CUT TO 
10 INCHES AND LACtD INTO HARNESS 

CONDUCTORS WITH THE SAME NUMBER ARE TWISTED TOGETnER 

INTERPkET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

MARK CHARACTERS .10 - *14 HIGH COLOR BLACK PER ND 1002019 AT 
LOCATIONS SHOWN 

LENGTHS SPECIFIED FOR CONDUCTORS ARE FOR AFTER TWISTING 


MANNED SIZE 

SPACECRAFT 

CENTER A 

HOUSTON, TEXAS 

SCALE-NONE REV LTR 




GOH 


WIRE HARNESS A 


1001474 


PENNANT GENERAL NOTES 

NOTE 

12 LENwTHa IN CONDUCTOR ChAHT ARt FOR REFERENCE ONLY 

13 SEE DETAILS B AND C ON CONF1GURAT1 ON SHEET FOR METHODS OF 
TERMINATING SHIELDS 

14 IDENTIFY USING DRAWING NO** REVISION LETTER AND MANUFACTURERS 
SYMBUL PER ND1002019 AND SERIALIZE PER N01002C23* 


GOH 

PENNANT 

NOTE 



WIRE HARNESS A 



1001474 


LIST OF MATERIALS 

ITEM OTY PART NO DESCRIPTION 

13 1 1010776- 3 WIRE* SHIELDED* 26AWG* 3 COND 1 FT *** IN* 

TOT. LG 4.0 

14 J 1000121 CONNECTOR* RECEPTACLE 

1$ 3 1000122 CONNECTOR* RECEPTACLE 

16 3 1010318- 1 CONNECTOR* PLUG 

17 1 1010472- 1 CONNECTOR* PLUG 

18 2 1000120 CONNECTOR. PLUG 

19 1 1001474- 11 SHIELD-WIRE* QQ-B-575* 17/64 I D 36AWGI* 

6*62 IN* LG 

20 1 1001474- 12 SHIELD-WIRE. QQ-B-575* (7/64 I D 36AWGI• 

9.00 IN* LG 

21 2 1001474- 13 SHIELD-WIRE* QQ-B-575* (7/64 I D 36AWG)• 

4*62 IN* LG 

22 1 1001474- 14 SHIELD-WIRE. QQ-B-575* (7/64 I D 36AWG)• 

18.50 IN* LG 

23 1 1001474- 15 SHIELD-WIRE* QQ-B-575* (7/64 I D 36AWGI* 

4*12 IN* LG 

24 AR 1010490-983 SLEEVING-HEAT SHRINK. WHT• 55 IN. TOT. LG 

WZ 

25 7 1010490-***. SLEEVING-HEAT SHRINK* 

26 7 1010490-058 SLEEVING-HEAT SHRINK. 

9 

27 -4X 1010490-084 SLEEVING-HEAT SHRINK* 































LIST OF MATERIALS 


ITEM 

28 

OTY 

12 

PART NO 

1000243- 5 

DESCRIPTION 

FERRULE* INNER 


29 



DELETED (1000242- 5) 


30 

130 

1006776- 18 

INSULATION* SLEEVING .31 

LG 

31 

49 

1006776- 16 

INSULATION* SLEEVING .31 

LG 

32 

8 

1010717- 1 

terminal LUG 


33 

1 

1000267 

BRACKET 


34 

1 

1000226 

BRACKET 


35 

1 

1000149 

BRACKET 


36 

AR 

QQ-S-571 

SOLDER (SN60MARP2) 


37 

AR 

MIL-T-713 

TAPE* NYLON* MAXED* TY®E 

P. 

~ 38 

9 

1010490-002 SLEEVING, HEAT SHRINK 


39 

24- 

1010490-080 

SLEEVING, HEAT SHRINK 



MANNIO SIZE 

SPACECRAFT 

CENTER A 

HOUSTON, TEXAS ” 

SCALE - NONE REV LTR 



1001474 

SHEET 6 OF 23 


























































GC'H 


IRE HARNEY L> A 


X D 


1474 





!■-«■•»§« 1 4". 1 “ll-JU 




































































































3 W 























































































































IMS'S 












































































































































































































lARNtSS A 


1001474 




SCALE-NONE 


GGH 


HcNNAN 
NOTE 
12 
13 


Oc'»c«Al -\CTc.j 


*I»E harness A 

* 


A 


LtNsjTHo IN CONDUCTOR CHART ARE FOR RtF ERtNCfc ONLY 

SEE DETAILS b AND C ON CONFIGUKATI ON SHEtT FOR METHODS OF 

terminating shields 

IDENTIFY USING DRAWING NO.# REVISION LETTER AND MANUFACTURERS 
SYMbOL PER ND 1002s-19 AND SERIALIZE PER N01Gu2023# 


1001474 


14 












GOH 

PENNANT 


LIST OF MATERIALS 


HIRE HARNESS A 


NOTE ITEM OT1 
1 

2 

3 

4 

9 

4 

7 

• 

♦ 

10 

11 

12 


PART NO 
1010416- 

1010416- 

1010414- 

1010416- 

1010416- 

1010414- 

1010416- 

1010416- 

1010416- 

1010416- 

1010776- 

1010776* 


1 

3 

9 

6 

7 

4 

6 

9 

10 

2 

1 

2 


DESCRIPTION 

WIRE* NIL-W-16878E28* 28AWG* BLK* 20 FT 
4*29 IN* TOT* LG 

WIRE* MIL-W-16878E28* 28AWG. RED* 11 FT 
11*12 IN* TOT* LG 

WIRE* MIL—W-16878E28• 28AWG* GY* 8 FT 9*66 IN* 
TOT* LG 

WIRE* MIL—W-16876E26* 28AWG* VIO* 7 FT 3*29 IN* 
TOT* LG 

WIRE* MIL-W-16878E28* 28AWG* BLU* 9 FT 6*79 IN* 
TOT* LG 

WIRE* MIL—W-16878E28. 28AWG* OWN* 6 FT 
10*29 IN* TOT* LG 

WIRE* MIL-W-16878E28. 28AWG* GRN* 29 FT 
7*13 IN* TOT* LG 


WIRE* MIL—W-16878E28* 28AWG* YEL* 22 FT 
4.79 IN* TOT* LG 

WIRE* MIL-W-16878E2S. 28AWG* WHT* 4 FT 
11*86 IN* TOT* LG 

WIRE* MIL-W-16676E28* 28AWG* BRN* 2 FT 6*79 IN* 
TOT* LG 

WIRE* SMIELDEO* 28AWG* 1 COND 9 FT 8*77 IN* 

TOT* LG 

WIRE* SHIELDED* 28AWG* 2 COND 10 FT 7*9 IN* 

TOT* LG 


MANNED 

SPACECRAFT 

CENTER 

HOUSTON, TEXAS 


SCALE-NONE 


SIZE 

A 


REV LTR 


A 


1001474 


|SHEET 




ML 


6QH ___WIRE HAR»ESS__A 

pennant LIST of materials 


ITEM OTY 

PART NO 

DESCRIPTION 

28 

12 

1000243- 9 

FERRULE* INNER 

29 



DELETED <1000242- 91 

30 

130 

1006776- 18 

INSULATION. SLEEVING .31 LG 

31 

49 

1006776- 14 

INSULATION* SLEEVIN6 *31 LG 

32 

8 

1010717- 1 

terminal LUG 

33 

1 

1000267 

BRACKET 

34 

1 

1000224 

BRACKET 

39 

1 

1000149 

BRACKET 

36 

AR 

00-S-971 

SOLDER < SN60WARP2) 

37 

AR 

MIL-T-713 

TAPE* NYLON* WAXED* TYPE P* CLASS 2* BLACK 

38 

9 

1010490-062 

SLEEVING* HEAT SHRINK 

39 

24 

1010490-080 

SLEEVING* HEAT SHRINK 


1001474 


MANNED 


SIZE 


SPACECRAFT 

CENTER A 

HOUSTON, TEXAS 


SCALE-NONE \ REV LTR 


& 


1001474 


SHEET 



GOH_ 


PENNANT 

NOTE ITEM OT 


_WIRE HARNESS 


LIST OF MATERIALS 

PART NO DESCRIPTION 


1010776- 3 

WIRE* SHIELDED* 28AWG* 3 COND 
TOT* LG 

1 FT 4*0 IN* 

1000121 

CONNECTOR* RECEPTACLE 


1000122 

CONNECTOR* RECEPTACLE 

, 

1010316- 1 

CONNECTOR* PLUG 


1010472- 1 

CONNECTOR* PLUG 


1000120 

CONNECTOR* PLUG 


1001474- 11 

SHIELD-WIRE* OO-B-979* <7/64 
6*62 IN* LG 

1 D 36AWGI* 

1001474- 12 

SHIELD-WIRE* OO-B-979. <7/64 
9*00 IN* LG 

I D 36AWGI* 

1001474- 13 

SHIELD-WIRE* OO-B-979* <7/64 
4*62 IN* LG 

I D 36AWG)* 

1001474- 14 

SHIELD-WIRE* OO-B-979* <7/64 
16*90 IN* L6 

I D 36AWGI* 

1001474- 19 

SHIELD-WIRE* OO-B-979* <7/64 
4*12 IN* LG 

I D 36AWGI* 

1010490-969 

SLECVING-HEAT SHRINK* WHT* 99 

• IN* TOT* LG 

1010490-112 

SLEEVING-HEAT SHRINK* 


1010490-098 

SLEEVING-HEAT SHRINK* 


1010490-084 

SLEEVING-HEAT SHRINK* 



MANNCO 

SPACECRAFT 

SIZE 


CENTER 
HOUSTON. TtXAS 

A 


SCALE-NONE 

REV LTR 



1001474 
I SHEET 










































WIRE HARNESS A 


MIRE HARNESS A 


CONDUCTOR 

I wot VI D UA L Li NGTH 

_ 

nu m uk [no. ^ 


cut Wl«f Ot SHIHO 

SHIP Will Ol JACK IT T 
CIICUIT POINT 1 * Hi 


CUT Will Ol SMIEU) 

SHIP Will Ol JACKIT P 1 <t> 
CIICUIT POINT 1 I n) . 


CONDUCTOR 

_INDIVIDUAL LI NOTH 

__ H (*> 

NUMBII I NO. 1 - 


CUT Will Ol SHI«0^ 

SHIP Will Ol JACKIT 7 

CIICUIT POIN T ] » 'l l 


__CUT *111 Ol SMIHO 

SHIP Will Ol JACKIT r 
CIICUIT POINT ] jD> 1 




P17 -F_ 

P17-C_ 

3 lj P18—V 
S12P18-P* 


2A SH LD A4 9 
_4_ P16-F_ 


A —59 12 

A 59A 1 


aoc__ 

25CSHL0 A39 


912P16-B*_ 
50( P16-Z 


3 87P18-W_ 

81P1 8-V 
887 P18-S 
887P1 8-U 
150SH LP AS6 
J2 I-17 
J21-18 
L287P16-L 


8 ld87P16-0 


A P 

a Ji*-s 

2 J1A-P 

2 J14-R_ 

2 P16-T 

2 J13-B_ 

2 J13-L L 
2 J13-NN 

2 J13-JJ 

E33_ 

87 P1 8-M 
^87 P18-U 

_2 C3- 2_ 

2 C 3- l 
2 P16-S 


A_39 K_ 

A_391_ 

A 80 1 

A 80R 

A 80K_ 

A_801 _ 

A 81 
♦ A 82 0 
A 820 
A 827 
A 8» 

A 68 
A 87 A 
A 870 
A 87F 
A 88 


_ E33_ 

_2 A18-_8_ 

_2 A1 4- 3 


23CSH LP A80 

_P18-F_ 

_ P18-C_ 

I2!P18-K_ 

225CP13-Y_ 

223CP 13-P* 
2 J 5 C P13-B*_ 


Hr*— 

2 Ui 8 - 2 


4 U14- 1 


_ 80CP15-S_ 

1 lkt SHLP A87 


J21“20_ 
J21-21 
| 202!P13-H 


2 A14- 5 
50 J14-N 

3 0 J14 -L_ 

50 J14-W 
5oj P15-T 
5 J P13-M 

_ E33 

87 P13-H 
87 P15-J 


29 21 30 
H ! 


sol J13-0 


MANNED 

SPACECRAFT 


r. ^TUI CONDUCTOR TERMINATION FIGURES ARE PER 


MANNED 

SPACECRAFT 

CENTER 


















GOH 


WIRE HARNESS A 


E 


1001474 



SHEET 






















































































































































































MOTES 

!• INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED E 

t UNLESS OTHERWISE SPECIFIED*. 

^ ALL OVER 

FILLETS AND RADII TO BE.062 

3. DENTIFY USING DRAWING NUMBER, REVISION LETTER, AND MANFA 
SYMBOL AT THE INDICATED LOCATION PER Mtl-STD-lBO. 

A. REMOVE BURRS AND BREAK ALL SHARP EDGES .OOSTOOIS R. 

5. LINE THRU CENTERS OF E53 AND S3 ESTABLISHES ! AXIS AZ 1 . 
ft. II $J. TOLERANCE apply in this area only. 

7. UNE THRU (KflS All AND CENTER OF ITEM (T) ESTABLISHES I 

& ALL DIMENSIONS MUST BE WITHIN SPECIFIED LIMITS AT A UNIFORI 
TEMPERATURE OF 68*F *I*F. 

9 SEE SHEET Z FOR DIMENSIONS OF ALL HOLES SHOWN 
NOT DIMENSIONED ON THIS SHEET. 















































































H 0 4 ( t/Z)- 40 NC -23 

. 2/0 t t/N fJH tho 
CS/ r W- 90 * 70 ./ 3 -./ 5 D/A 
eno es 
EZ2SI 


-NO. 4 (.H 2 )- 40 NC-e& 

.200 M/N FULL THO 

CSC SO*- 90 * TO. ! 3~./5 D/A 

/HOLE 


~ pcoepw# - no cpmnsc 
C-; /sst/e _ 


fS G&yP 

S*U 


N0.4(//E)-40NC-EB THPU « 
CSC SO *- 90° TO. I3-./5 D/A 


-J8S-./90D/A SLOT 
OH /.07b/? BSC 

3 PE AC SHAPP 5DOFS .0/0-.020 


3 PLACES 



4S*PEF 


^.-■2^-40 kC-23 *- 

•? Y t •*. .4 ~*f D 
30*-9C*~C ./3-./&W* 
?.rS 




PAPT/AL SECT/ON S"S 



. 250 —■ 
2 PLACES 


-030 BSC 


2.873 
2 PLACES 


■ HO. 4( H2)-40 HC ZB 
.200 MIN FULL THD 
CS/T 30°-90“ T0./3-./5 D/A 
3 HOLES 

ON 2.500 D/A 8SC 


PAPT/AL SECT/ON K-K 


NO. 4(HZ)- 40HC-28 -v 

.200 M/N FULL THD ' 

CSC 80*-90*-./3'J3D/A 


N0.2(i3t)-S*NC-2B -THtU^ 
CSC 8C'-90~ TO J/-./3D/A 
4 HOLES 


-.520 BSC 


-N0.4(t/2)-40NC -23 
2HOLES MAPCED A‘.200M/N FULL THD 
2 HOLES MAPPED “3“ THPU 
CSC80*- 9O* TO J3-J0 D/A 


N0.4 ( //2)' 40NC-2B - 

.200 MIN FULL THD 
CSC 80*-90 * T0./3-./6 D/A 
3 HOLES 

ON2.500 D/A 8SC 


■ N04(flt)-40NC-28-TH2U 
CSC 80 m -90°TO. /3 /S D/A 
v 2 HOLES 


r HO. 2(. 03b) - 5b NC -23 THPU 
' CSC 80“-7CfTQ .//-,/3 D/A 


4 HOLES 


-J88 BSC 


-HO. 2(. 08b}5bNC-2B- THPU 
CSC SO *-90 “ TO J/-./3 D/A 
ZHOLES 



2.000 ,] 750 


-HO. 4(. HE) - 40 HC -2B 
.200 M/H FULL THD 
CSC80°-90* 70J3-./5D/A 
2 HOLES 


NO. 4(.//2)-40HC - 28 - 

.200 M/N FULL THD 
CSC 80*- 90° TO./3-. /5 D/A 
4 HOLES 

m.uuso/4 


, P TTPNCAL - 


ALL EDGES tOf SLOT 


- HO. pf. 08b)-5b HC-2B-THPU 
CSC 80 •- 90° TO J/-./3 D/A 
2 HOLES 


NO. 4(.//2) - 40 NC - 23 - 

.200 Ni/N FULL THD 
CSC 80°-90“ TO J3-./5D/A 



“%« / 00 ° 
t'£L BSC 

BSC | 


-NO,4( //Z)-40HC-23 
.200 M/H FULL THD 
CSC 80*-90* TO. /3 -,/SD/A 
2 HOLES 


- HO. 2(. 03b)-5b HC -2B - THBU 
CSC 80*-90*70 .//- J3 D/A 
2 HOLES 


H0.4(. HE) - 40 HC -23 - THPU 
CSC 80*-90* TO ./3-./5D/A 
2 HOLES 


.8/2 \f.954~ 
8SC BSC A 


-N0.4(.//?)- 40 HC-28-THPU 
CSC 80°-90° T0./3-./SD/A 
2 HOLES 


.O/ /p —. 
.03 

2 PLACES 



R^rTwMi 


- NO. 2(. 03b) - 6b NC -23 
/ HOLE MAPPED “A “.200 M/N FULL THD 
3 HOIES MAPPED "8" THPU 
CSP 80*-90* TO J/-./3 D/A 


PACT/A L SECTION R-R 
SCALE 4:/ 

4 PLACES 


- NO. 4(- HE)-40NC -23 - THPU 
CSC 80*- 90“ TO . /3 /S D/A 
2 HOLES 


MANNED 

SPACECRAFT CENTER 
HOUSTON. TEXAS 


-./38 BSC 


- HO. 4(. H2)-40HC-23 
.200 M/N FULL THD / J 
CSC eo°-9O 0 TO J3'./4 D/A 
2 HOLES 


+ + ... £J**S4 

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STABLE MEMBER. 


DO NOT SCALE THS DRAWING lAPmWAL- 


0014: 


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(001478 


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3 


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•||| DIATHRl^ 
6 HOLES EQUALLY 
SPACED ON 1.750 DIA BSC 

1-0-A.OOS DIa! 


-4 (.U2) - 40NC-2B THRU 
85* 15° CSK TO 

3 HOLES EQUALLY SPACED 
ON 1.687 DIA BSC 


A .005 DIA 


.04 O. 
.050 

.040 y 4.C*t 
.050 * 1 3 \ 


I® A .005 TIRl 


SEE NOTE 4- 


' /> 


2.130 n i a 

2.120 DIA 


1.330, 


LOOS 

.935 


.015 R MAX- 



90 t I 


NOTES 

_ I. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327 

2. 6 ?/ FINISH""UNLESS OTHERWISE SPECIFIED Qpr 

^ OOT otA 

3. BREAK ALL SHARP EDGES q, J R 

4. IDENTIFY USING DRAWING NO., REVISION LETTER AND 
MANUFACTURERS SYMBOL AT THE INDICATED LOCATION PER NDI0020I9 


revisions 7~DRP II2)( 


DR CHK DATE | APPROVED 


-.015 R MAX 


.005 R MAX 


till »*A 

EE] 


I <8) A .005 tTr 


>5 9 ± 5 ° 



.020 v 45°♦ 5 0 

.040 * 


SECTION A-A 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES INSTF 

CAPACITOR VALUES ARE IN < 

RESISTOR VALUES ARE IN OHMS —— 

TOLERANCES ON DRAWN jj 

FRACTIONS DECIMALS ANGLES CHECKED 

DO NOT SCALE THIS DRAWING APPROVE! 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


1001510 

1001508 


DL1001500 


material: TITANIUM 
ALLOY BAR,6AL-4V 
CLASS 5, PER 
MIL-T-3047 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


RETAINER, BEARING 

INNER AND MIDDLE AXIS 


APPROVED I 
MIT J 


APPLICATION 




CODE IDCNT NO. SIZE 


| SCALE 2 / I 


DRAWING NO. 


1001481 
































SEE NOTE 2D 



1.105 

|A .005 TIRI 


.015 R MAX 



I.I8T 
DIA MAX 


PIT] 1.000 

DIA MIN 


1.3123 uu 

EE] 


„ .270 - 


-OUTSIDE FACES TO BE 
FLUSH WITHIN .001 


NOTES 

I. GENERAL 

v A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-T0327 

^ " B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISION SPECIFIED IN NDIOI5404 CLASS 2 

G. IDENTIFY USING DWG NO., REVISION LETTER, MANUFACTURERS NAME OR SYMBOL, AND DATE OF 
PACKAGING PER NDI0020I9. MANUFACTURERS PART NO. MAY BE INCLUDED 
: 0. PACKAGING TO MEET REQUIREMENTS OF MIL-B-I97C METHOD IA-8 EXCEPT .004 THK 

POLYETHYLENE BAG FOR INITIAL WRAP MAY BE USED 


2. PERFORMANCE AND INSPECTION REQUIREMENTS 

A. DUPLEX PAIR, DF MOUNTED 

B. AXIAL YIELD RATE: 7 MICRO INCHES/LB MAXIMUM IN UNMOUNTED CONDITION 

C. MAXIMUM STARTING TORQUE : 3.0 O Z-1N U NMOUNT ED CO NDITION 

D. HIGH POINT OF ECCENTRICITY OF DIA | -A- | AND DIA |-B- I BOTH BEARINGS TO BE 
PERMANENTLY MARKED ON OUTBOARD FACES OF BOTH RACES 

E. LUBRICATE USING OIL MEETING REQUIREMENT OF MIL-L-G08S 

F. DIMENSIONS AND TOLERANCES DEFINED BY AFBMA STANDARDS UNLESS OTHERWISE SPECIFIED 

1. RADIAL RUNOUT : .0002 MAX 

2. SIDE PARALLISM: .0002 MAX 

3. SIDE RUNOUT WITH BORE: .0003 MAX 

4. GROOVE RUNOUT WITH SIDES .0003 MAX 

5. TAPER, O. D. AND BORE:.0002 MAX 

3. DESIGN REQUIREMENTS 

A. MINIMUM AXIAL LOAD CAPACITY: 450 LBS 

B. MINIMUM RADIAL LOAD CAPACITY: 100 LBS 

C. MAXIMUM STARTING TORQUE: 20 02-IN WITH 400 LBS AXIAL PLUS 20 LBS RADIAL 
LOAD IN UNMOUNTED CONDITION 

a MATERIAL* RINGS AND BALLS CRES 440C RC55 MIN HARDNESS RETAINER NON FUNGUS NUTRIENT 


2 


1 


L 


revisions TtX?R 1IZA£> 


OR I CHK I PATE | AAAAOVTO 



SEE NOTE 2D 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND1002034 FOR THIS DRAWING 


SSo 

PART OR 

MATERIAL 

NOMENCLATURE OR 

FINO 

IDENTIFYING NO. 

OR NOTES 

DESCRIPTION 

NO. | 










1001510 


1001508 


1001506 

DLI00I500 

NEXT ASSY 

USED ON 

| APPLICATION | 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN pi 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES | 


00 NOT SCALE THIS DRAWING 


SEE NOTE 3D 


MIT 

INSTRUMENTATION LAS 

CAMRRIOOC. MAS*. 


DRAWN 


mk 


APPROVED /.I 
MIT JcL 



T-lt-w 


4LL 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON. TOMS 


BEARING, BALL 
DUPLEX, SPECIAL 


SPECIFICATION CONTROL DRAWING 


COOE IOCNT NO. 


SCALE 2/1 


DRAWING NO. 

1001483 

| SHEET 




i 

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It 


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m-ti 

V'P! 


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-■ ;■ 

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REQUIREMENTS 
L GENERAL 

A.WTERPRET ORAWNG IN ACCORDANCE WITH MIL-0-70327 

a 2 

MANUFACTURERS NAM~ AND RARl NO ivuW~ OL VsJCLUOED 
2. INSPECTION* f ACCEPTANCE (lOO>Q 
A. ELECTRICAL rcouwements 

1 ELECTRICAL RATING- 3 AMPS #30VDC 

2 SWITCH ACTION-SPST OPENS ON TEMPERATURE RISE 
1 TEMPERATURE SETTING* I37*F OjOSlNG TEMPERATURE 
4 TEMPERAruRE SETTWG TOLERANCE: 13 * F 

& TEN'PERATURE DEFERENTIAL* 2*5* F 
A UCCHAMOH. REOURENENTS 

1 ALL DIMENSIONS MUST MEET REQUIREI4ENT5 CONTANGO ON THIS DRAWING 

2 BREAK ALL SHARP EDGES 
3L DESIGN REQUIREMENTS 

A. CONTACTS-SILVER PFR MIL-S-19424 


mry 


PJ04 


L i O06 



p-*pMO-So8 

♦Lasux* 

Tl |V?* 

ruph 


U L-D7^>'5 


lUdSs 


.Ay opA J 

MAX ^ 


I DAStOCS 


090 OA 1 w 1 


l X*5*XX5 
^^tOCB 


-J L—£) 78 tDl5 


cm 


-063 DIA THIU 
2 PLACES 


a 




2S0 

1 


-J2S 


JiSsU 


a Tl-ERMOSTAT HOUSING: NICKEL PLATE PER QQ-N *290 TYPE DT CLASS2 
C MWMUM OPERATING LFE AT OPERATING CONDITIONS* 50.000 CYCLES 
Q MOUMTWG BRACKET t T^CRMOSTAT MAY RE SEPARABLE 

E. UNITS '^'LL BE CAPABLE CF Y\lT-isTLKini!.r tul * * ■ »/viNC ENVIRONMENTAL STRESSS^ 


- Sk lL BE CAPABLE CF WITHSTANDING THE F> 11 
I TEMPERATURE :-6ST 70 340T (NON* OPE RATING) 

P viiyratihm* i 5—20C 0 CPS AT IOG OR 
Z. VIBRATE. (5 . S00 CFS AT |S0 (OPERATING) 

S SHCCK. MlL-£-52^2C RMIAGRAFH 4.I5.SI (N0N-CPEN4TING) 

4. ACCELERATION; MIL-E-5272C PARAGRAPH 4.16.3 (NC N- OPERATING) 

F. THERMOSTAT BRACKET; STAINlESS STEEL, P^SriVA.TD PER MIL* F*14072 FINE* 300 
G* VOLTAGE DROP ACROSS TERMINAL 45 MV MAX f> 3 AMPS 


a? a {si? a 


. # • r *. m- m* §% 

4 I f PROCURE l)NLf-FROM ^APPROVED 
- 1 4 J ‘ • 3D XM NDI0C2O34 

F'R f Hl*I DRAWING 


REPLACED WITHOUT CHANGE 
BY REV M B" PER TDRR 30733 


ii^ DUa .".E£ iOPUCATIifl 

'usmarimu 


: / s. 




i— ■■- . TT T _ t< ^ - 






~^ ♦ 0 C 6 ^ 


6 l 1000201 

W ■** KMI M« MMI 

1000005 

OLIOOOOOI 

MWl 

mm mm 

mmm 


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■W 


•— me 7^ 
‘— 


•"/?* MWMi | m' 


LIST Of PMT» ANQ MXTtPMUJ 


I mmvm i | w 


THERMOSTAT; 

SAFETY 


tygnCATION CONTPQt. QRAWlNt* 


2/i 


p^rTTam 


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MarmwtNTtmiK 
UK)»*T W T 


100148 S 


1001465 














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^J4tDlO 


1*05 
-£390 DlA- 


REQUIREMEN1TS r; 

U GENERAL .._JI 

A. INTERPRET DRAWING IN ACCORDANCE WITH MIL-0* 70327 

a SUPPLER SHALL CONFORM TO THE QUALITY ASS^ANCE < -*1.275 I 

PROVISIONS SPECIFIED IN NASA SPEC ND1015404 CLASS 2 | 

C IDENTIFV USING DRAWING NO, REVISION LETTER.SERIAL Na^ U-550-iJ 

MANUFACTURERS SYMBOL AT PER MIL-STD-130 . ^ MN . n 

MANUFACTURERS NAME AND PARI NQ ivu*-bt IMCLUOED - 

2. INSPECTION* f ACCEPTANCE (lOOX) « 

A. EL0CTRICAL REQUIREMENTS MA 

i ELECTRICAL RATING- 3 AMPS «30VDC 

2. SWITCH ACTION-SPST OPENS ON TEMPERATURE RISE 

3. TEMPERATURE SETTING* I37*F CLOSING TEMPERATURE 

4. TEMPERATURE SETTING TOLERANCE: i3*F 
& TEMPERATURE OFFERENTIAL: 2-5* F 

a MECHANICAL REQUIREMENTS 

l ALL DIMENSIONS MUST MEET REQUIREMENTS CONTAINED ON THIS DRAWING 
2. BREAK ALL SHARP EDGES 
3L DESIGN REQUIREMENTS 

A. CONTACTS-SILVER PER MIL-S-19424 

a THERMOSTAT HOUSING: NICKEL PLATE PER QQ-N -290 TYPE Iff CLASS2 
C MINIMUM OPERATING LFE AT OPERATING CONDITIONS, 50,000 CYCLES 
Q MOUNTING BRACKET ( THERMOSTAT MAY BE SEPARABLE 

E, UNITS SHALL BE CAPABLE CF WITHSTANDING THE FOLLOWING ENVIRONMENTAL STRESSES 
t TEMPERATURE:-65*F TO 340T (NON-OPERATING) 

* wnDAT,™; *5-2000 CPS AT IOG OR 
z VIBRATION* (5.30Q C PS AT I5G (OPERATING) 
a SHOCK: M1L*£-'5272C PARAGRAPH* 4.I5.SI (NON-OPERATINGT 
-HTACCELERATION MIL-E-5272C PARAGRAPH 4.16.3 (NON-OPERATING) 

F. THERMOSTAT BRACKET ; STAINLESS STEEL, PASSIVATED PER MIL-F-14072 FINE- 300 _ 

“6. “VOLTAGE DROP ACROSS TERMINAL 45MVMAX6? 3 AMPS 


k-oie ±£X5 

78*> 15 



-J063 DIA THRU 
2 PLACES 



PFmJREnmXTFROM J^PPRO VE D 
SOURCES LISTED ~0F£INDIQC2Q34 
“F r JR THIS DRAWING 


LIST Of PARTS ANO MATERIALS 

THERMOSTAX 

SAFETY 


. spacecraft cemte* 


DLI00020I oo" 

1000005 puoooooi 


MT/IL AffAOVAL | CAT! | 


6JFICATI0N CONTROL DRAWING -- 

**a umit wt. coot ioemt. )Q0I485 

2 /i SHEET 1 OF 1 SHEET 






















REQUIREMENTS: 

1. general 

A. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

B. SUPPLIER SHALL CONFORM TO THE QUALITY ASSURANCE PROVISIONS 
SPECIFIED IN NASA SPEC NDI0I5404 CLASS 2. 

C. IDENTIFY USING DRAWING NO., REVISION LETTER, SERIAL NO-, AND 
MANUFACTURERS SYMBOL PER MIL-STD-130. 

MANUFACTURERS NAME AND PART NO MAY BE INCLUDED. 

2. INSPECTION AND ACCEPTANCE (100%) 

A. ELECTRICAL REQUIREMENTS 

1. ELECTRICAL RATING - 3 AMPS • 30 VDC. 

2. SWITCH ACTION-SPST OPENS ON TEMPERATURE RISE. 

3. TEMPERATURE SETTING: 137° F CLOSING TEMPERATURE 

4. TEMPERATURE SETTING TOLERANCE ±3°F. 

5. TEMPERATURE DIFFERENTIAL: 2°-5 # F. 

B. MECHANICAL REQUIREMENTS 

I. ALL DIMENSIONS MUST MEET REQUIREMENTS CONTAINED ON THIS 
DRAWING. 

2 BREAK ALL SHARP EDGES. 

3. DESIGN REQUIREMENTS 

A. CONTACTS - SILVER PER MIL-S-19424. 

B. THERMOSTAT HOUSING NICKEL PLATE PER QQ-N-290 TYPE BE CLASS 2 

C. MINIMUM OPERATING LIFE AT OPERATING CONDITIONS'- 50000 CYCLES 
D- MOUNTING BRACKET AND THERMOSTAT MAY BE SEPARABLE. 

E. UNITS SHALL BE CAPABLE OF WITHSTANDING THE FOLLOWING ENVIRON¬ 
MENTAL STRESSES: 

I. TEMPERATURE: -65°F TO 340*F (NON-OPERATING). 

2 VIBRATION: 5-2000 CPS AT 10 G OR 

5 - 500 CPS AT 15 G (OPERATING). 

3 SHOCK: MIL-E -52720 PARAGRAPH 415-5.1 (NON-OPERATING). 

4. ACCELERATION: MIL-E-52720 PARAGRAPH 4.16.3 (NON-OPERATING). 
F THERMOSTAT BRACKET: STAINLESS STEEL, PASSIVATED PER MIL-F-l4072 
FIN E- 300. 

G. VOLTAGE DROP ACROSS TERMINAL 45 MV MAX AT 3 AMPS. 


£ 

r 


• 03i -;8oo 


.937 


±.007 


- + 007 

031 -.000 


.275 


±.004 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON NO 1002034 
FOR THIS DRAWING. 


$9*1001 


3 


2 


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loee oo ^3 


DESCRIPTION 


REPLACES REV "A" WITHOUT 
CHAN6E PER TPRR 30733 


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66 1 




APPROVED 













DL1000201 

•000005 

DLI000001 

NEXT ASSY 

USED ON 

1 APPLICATION I 


UNLESS OTHERWISE SPECIFIED 


2 PLACE 3 PLACE 
lOECIMALS DECIMALS ANGLES| 

+ 005 + 


DO NOT SCALE THIS DRAWING 


■ U I T- 

INSTRUMENTATION LAN 




wmm S-A-HOFF 30MAY64I 


CONTRACT NAS 9- 153 


J.BARNARD 

NASA APPROVAL_ 


W. KUPFER 9/3/64 

MIT APPROVAL_ 


MANNED 

SPACECRAFT CENTER 
HOUSTON. TEXAS 


THERMOSTAT, SAFETY 

SPECIFICATION CONTROL DRAWING 


COOE WENT NO. 




1001485 


iSHEET 
















J__!_I_ 1 _ I 5 1 


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2. SWITCH ACTION-SPST OPENS ON TEMPERATURE RISE 
3L TEMPERATURE SETTING* I37*F CLOSING TEMPERATURE 
4 . TEMPERATURE SETTNG TOLERANCE* ±3*F 
SL TEMPERATURE DEFERENTIAL* 2^5* F 
B MECHANICAL REQUIREMENTS 

L ALL DIMENSIONS MUST MEET REQUIREMENTS CONTAINED ON THIS DRAWING 
2. BREAK ALL SHARP EDGES 
31 . DESIGN REQUREMENTS 

A. CONTACTS-SILVER PER MIL-S~ 19424 


& THERMOSTAT HOUSING: NICKEL PLATE PER QQ-N -290 TYPE BT CLASS2 
C MNIMUM OPERATING LFE AT OPERATING CONDITIONS, 250,000 OCLE5 
Q MOUNTING BRACKET ( THERMOSTAT. MAY BE SEPARABLE 

E, UNITS SHALL BE CAPABLE OF WITHSTANDING THE FOLLOWING ENVIRONMENTAL STRESSE5 

C TEMPERATURE:-65V TO 340T (NON-OPERATING) 

. 2 VIBRATION-* tS-20CQ CPS AT 10G OR 
Z VIBRATION. (S _ $0Q cps AT gg (0PERAT|NG) 

a SHOCK! MiL^E-*5272C PARAGRAPH 4.IS.SI (NON-OPERATINGt 

; ACCELERATION: MIL-E-5272C PARAGRAPH 4J6.3 (NON-OPERATING) f 

F, THERMOSTAT BRACKET; STAINLESS STEEL, PASSIVATED PER MIL-F-14072 FIN E-300 


"SOURCES LISTED -mzTOQQ2034 
TOR THIS DRAWING 



DLI00020I 


IQQ00Q5 IDLIQOOOOI 


nucnoNt occmmu tm us 
1035 Oo 




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PHOTOGRAPHIC SCALE ONLY 

k __ . . ,**. 


- 

QTV. NOMCNCLATUM | PART OR —nr.-rmn.. 1 MATCRIM. T RNO 

«*Q0 or octcRtmoN 1 lOommuQ no. wwhcation | m N0Tn | m 

LIST OF PARTS AND MATERIALS 

MIT 

MRfRWMCMTATIOM IM 

MAS *-153 |W 

THERMOSTAT 

MIT 

INSTRUMENTATION 

LAOORATOWT 


m> «a 


SAFETY 

•MMO 

mm MSC / 

5PBDFICATI0N OONTROL DRAWING 

VNCCCMAfT CiNTIII 
HOuaroM mma 

* MT^L AMROVM. | OATC 

JiJ 1 r /tl M 

kmi umt »r. cm non. 

2 /l 

1001485* 

ris,. ifjfr 

- 1 - ' I - 

«M«T l OF 1 SHEET 


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2 


m I 


6 T J H_A_D_ SCREW I 

MIN MIN MAXlMIN MAXlMIN MAxl MIN SIZE 

,028 .038 .078 .086 .083 ,140 |.I34 .086 p822j 2-56UNC-3A 

.036 ]p5l .094 ,112 .108 .183 .i73 .112 ,10 

,044 .064.109 .138 .134 . 226 .218 .138 .13: 

.052 .0771.141 .164 .159 .270 .262 164 J585|8-32UNC-3A| 29 

.061 ,090l.i56~.l90 .185 .312 13031.190 jj84 >0-32UNF-3A ~ 


LENGTH L ±015 __ 

.3751.4381.500l.562l.6251.687|.7501-812 |.8751.937ll.00C 


^ _ REVISIONS TDRR Og7Q __ 

ZONE I SYM DESCRIPTION DATE I APPROVAL 

A REVISED PER TDRR 13948 ll~\UA U<- 




5 

6 

7 

8 

9 

10 

II 

12 

13 

14 

19 

20 

21 

22 

23 

24 

25 

26 

27 

28 

33 

34 

35 

36 

371 

38 

39 

40 

41 

42 

47 

48 

49 

50 

51 

52 

53 

54 

55 

56 





SEE NOTE 2D 


REQUIREMENT^* 

1. general; 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN 
NDI0I5404 CLASS 3 

C. IDENTIFY USING DWG NO., APPLICABLE DASH N0.,REVISI0N LETTER 8 MANUFACTURERS 
SYMBOL PER ND 1002019. MANUFACTURERS NAME 8 PART NO. MAY ALSO BE USED 

D. SCREWS SHALL MEET ALL REQUIREMENTS OF FF-S-86 TYPE 2ZT EXCEPT AS SPECIFIED BELOW 

2. DESIGN REQUIREMENTS: 

A. MATERIAL:SCREW; 410 CRES PER MIL-S-862 CLASS 3 . 

INSERT: GREEN POLYCAP NYLON PER QPL18240 

B. FINISH:SCREWs PASSIVATE PER MIL-F-14072 FIN E-300 

C. HARDNESS: SCREW; Rc 38-43 

D. insert: 

I.SHALL MEET THE REQUIREMENTS OF MIL-F-18240 TYPE B 

E. DIMENSIONS: AS SHOWN ON DELINEATION 8 CHART 

F. SCREW SHALL BE FREE OF ALL BURRS 

G. SCREW HEAD 8 SOCKET TO BE FORMED BY COLD-HEADING. THREADS TO BE 
FORMED BY ROLLING 

3.SCREWS MAY BE MADE FROM NASA DWG NO. 1001489 


PROCURE ONLY FROM APPROVED SOURCES 
LISTED IN ND 1002034 FOR THIS DRAWING 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


MULTIPLE _ 

USAGE _ 

NEXT ASSY USED ON 

APPLICATION 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


SEE NOTE 2 A 


M I T 

INSTRUMENTATION LAB 

CONTRACT 

_ NAS 9 153 ["date ' 

approved JQMvtA ' 

CHECKED I ’ ** 

OPAWN ilflUCHg 111/? 17^3 
MLT/IL APPROVAL I DATE 


LIST OF PARTS AND MATERIALS 

SCREW 

HEX SOCKET HEAD 
SELF LOCKING 

SPECIFICATION CONTROL DRAWING 

SCALE I UNIT WT. | CODE I DENT. 


INSTRUMENTATION 

LABORATORY 

Camdrip—. Mam. 

pro. MO. _ 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001488 


3 

























G T J H A _ D SCREW LENGTH L±0I5 

MIN MIN _ MAXlMIN MAX l MIN MAX 1 MIN SIZE ~I87 | .250] 312 1.3751.438 |.5Qol.562|.625 1 .687 1 .7501.812 1.875 1 .937 ll.OOC 

.028 .038 078 .086 .083 .140 .134 .086 p822 £- 5«i JNC-3A 

036 051 .094.112 .108 .183 .176 .112 , 10754 40UNC-31 12 3 4 5 6_7 8 9 10 II 12 13 14 

044 064.109 .138 J34 .226.218 .138 J3296-32UNC-3A 15 16 17 18 19 20 21 22 23 24 25 26 27 28 

052 077 .I4T.I64 .159 ,270 .262 .164 J5858-32UNC-3A 29 30 31 32 33 34 35 36 37 38 39 40 41 42 

061 .090.156 .190 .185 .312 303 .190 J84 I0-32UNF-3A 43 44 45 46 47 48 49 50 51 52 53 54 55 56 


ZONE SYM 


REVISIONS TDRR 08763 
DESCRIPTION I DATE I APPROVAL* 




SEE NOTE 2D 


REQUIREMENTS* 

1. general; 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN 
ND1015404 CLASS 3 

C. IDENTIFY USING DWG NO., APPLICABLE DASH NO.,REVISION LETTER a MANUFACTURERS 
SYMBOL PER ND 1002019. MANUFACTURERS NAME 8 PART NO. MAY ALSO BE USED 

D. SCREWS SHALL MEET ALL REQUIREMENTS OF FF-86 EXCEPT AS SPECIFIED BELOW 

2. DESIGN REQUIREMENTS: 

A. MATERIAL: SCREW \ 410 CRES PER MIL-S-862 CLASS 3 

INSERT: GREEN POLYCAP NYLON PER QPL18240 

B. FINISHlSCREWi PASSIVATE PER MIL-FH4072 FIN E-300 

C. HARDNESS: SCREW; Rc 38-43 

D. insert: 

(.SHALL MEET THE REQUIREMENTS OF MIL-F-18240 TYPE B 


E. DIMENSIONS: AS SHOWN ON DELINEATION 8 CHART 

F. SCREW SHALL BE FREE OF ALL BURRS 

G. SCREW HEAD 8 SOCKET TO BE FORMED BY COLD-HEADING. THREADS TO BE 
FORMED BY ROLLING 

3.SCREWS MAY BE MADE FROM NASA DWG NO. 1001489 


PROCURE ONLY FROM APPROVED SOURCES 
LISTED IN ND 1002034 FOR THIS DRAWING 


MULTIPLE 

USAGE _ 

NEXT ASSY USED ON 

APPLICATION 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO 


SPECIFICATION 


MATERIAL 
0* NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 

SEE NOTE 2 A 


M I T 

INSTRUMENTATION LAG 
CONTRACT 

_ has 9-153 ranr 

CHECKED I I 


is 


MIT/IL APPROVAL 


LIST OF PARTS AND MATERIALS 

SCREW ' 

HEX SOCKET HEAD 
SELF LOCKING 

SPECIFICATION CONTROL DRAWING 

SCALE I UNIT WT. I CODE IDENT. 


INSTRUMENTATION 

LABORATORY 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

1001488 


INCHES 


[-mmmmmnmwcMENmsr 






















H 


MAX MIN 




LENGTH L *.015 


.312 


2-56UNC-3A 




.061 l.Q9ol.l5ff 1.1301.185 1.312 1.3031.190 [.IS4- H)0-32UNF-3A 43 44 45 46 47 48 [ 43 1 5~0 | 51 | 52 ~53| 54-| 55 | 5£ S7 



2 

3 

mi 

imi 

5 

111 

7 

16 

17 

13 

EEI 

21 

30 

44 

31 

45 

32 

46 

33 

47 

34 

48, 

35 

43 


REVISIONS TV R R 0 9 76% 


DESCRIPTION | DATE 


REVISED PER TDRR 14791 


REVISED PER TDRR 19918 


APPROVAL 


w 


^ Mt-o. 

OTL s ju 


REQUIREMENTS 
U GENERAL: 

A. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS 
SPECIFIED IN ND1015404 CLASS 3 

C. IDENTIFY USING DRAWING NUMBER, APPLICABLE DASH NO. , REVISION 
LETTER £ MANUFACTURERS SYMBOL. PER ND 1002019 MANUFACTURERS 
NAME AND PART NO. MAY ALSO BE USED. 

. D. UNLESS OTHERWISE SPECIFIED SCREWS MUST MEET REQUIREMENTS 
~“~ OF FF-S-86 TYPE VL 

2.. INSPECTION £ ACCEPTANCE. 

A. MATERIAL.*410 CRES PER MIL-5-662 CLASS 3 

B. FINISH-' PASSIVATE PER MIL-F-14072 FIN E-30C 

C. HARDNESS- R f 36-45 

3. DESIGN REQUIREMENTS: I 

A. SCREW HEAD ^ SOCKET TO BE FORMED BY COLD 

HEADING. THREADS 10 BE FORMED BY ROLLINS - 


PROCURE ONLY FROM APPROVED SOURCES 
LISTED IN NDIOO2.034 FOR THIS DRAWING 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


multiple 

USAGE _ 

NEXT ASSY US 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


MIT I 

INSTRUMENTATION LAS I 

CONTRACT 1 

_ NAS 9-153 ["'date ' 

APPROVED 
CHECKED | 

drawn. IDTB- I \gI2AJg> 

MIT/H. APPROVAL I DATE 




LIST OF PARTS AND MATERIALS 

SCREW 

-HEX SOC HD 

SPECIFICAT/ON CONTROL DWG 

SCALE I UNIT WT. CODE IOENT. 

— 80230 


INSTRUMENTATION 
LABORATORY 
Camrrioor. MA—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001483 

SHEET \ OF | 




















































G T I J _A_ 

MIN MIN _ MAX ImiN MAX. [m'N MAX MIN S'ZE 

.023 .038 -076 .086 .063 .140 .134- .086 .0622 2-56UNC-3A 

.036 .051 .034 ."2 .106 163 .176 ,112 .1075 4-40UNC-3A 

.044 .064- .109 .138 .134 .226.216 J36 .1323 6-32UNC-3A 


.181 

250 

.312 

.375 

.438 

.500 

.562 

.625 

CT) 

CO 

-4 

o 

lo 

h; 

.812 

.875 

.937 

1.000 

1 

~Z~ 

3 

4 

5 

e 

7 

8 

9 

10 

II 

12 

13 

14 

15 

16 

11 

18 

13 

20 

21 

22 

23 

24 

25 

2€ 

27 

28 

23 

30. 

31 

32 

33 

34 

35 

36 

37 

3fi 

33 

40 

41 

42 

f-4 3 

44 

' 45 

46 

lii 

48 

43 

50 

51 

52 

53 

54 

55 

56 


REVISIONS . w _ 

■lent | SYM~ _ DESCRIPTION _ DATE APPROVAL 

A REVISED PER TDRR 14791 ,>-»»•*■ t M( 

B REVISED PER TDRR 19313 

C REVISED PER TDRR 20629 pjgi 




| | D. 

it s jtt 


REQUIREMENTS 
I. GENERAL: 

A. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS 
SPECIFIED IN NDIOI5404 CLASS 3 

C. IDENTIFY USING DRAWING NUMBER, APPLICABLE DASH NO. , REVISION 
LETTER $ MANUFACTURERS SYMBOL PER ND1002019 MANUFACTURERS 

~ NAME AND PART NO. MAY ALSO BE USED. 

D. UNLESS OTHERWISE SPECIFIED SCREWS MUST MEET REQUIREMENTS 
OF FF-S-86 TYPE VL 


2. INSPECTION £ ACCEPTANCE. 

A. MATERIAL : 410 CRES PER MIL-5-862 CLASS 3 

B. FINISH: PASSIWE PER M'L-F-14072 FIN E-30C 

C. HARDNESS’- R*38-43 

3. DESIGN REQUIREMENTS: 

A. SCREW HEAD $ SOCKET TO BE FORMED BY COLD 
HEADING. THREADS TO BE FORMED BY ROLLING. 
ALTERNATES SOCKET MAY BE BROACHED IN ACCORDANCE 
WITH THE REQUIREMENTS OF FF-S-.86; ffROVHD£ 0*-ALL 
BROACHING CHIPS ARE REMOVED, j : • 


PROCURE ONLY FROM APPROVED SOURCES 
LISTED IN NDI00a034 FOR THIS DRAWING 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


MULTIPLE 

USAGE _ 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M I T 

INSTRUMENTATION LAB 
CONTRACT 

_ NAS 9153 rbATE ' 

CHECKED ^ _____ 

drawn. |dtBj ~ mIzaJq 

AffRO^tD Xa MSQL t . 


MIT/jL APPROVAL DATE 

1 " J '''TB 


LIST OF PARTS AND MATERIALS 

SCREW 

HEX SOC HD 

SPECIFICATION CONTROL DWG 

i _,_,--- 

SCALE UNIT WT. CODE IDENT. 

- 80230 


INSTRUMENTATION 
LABORATORY 
Camrripor, Ma—. 

OWQ. NO. _ 

MANNED 

SPACECRAFT CENTER 

_ HOUSTON TEXAS 

NASA DRAWING NO. 

1001480 

SHEET 1 OF | 


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7 

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13 

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5 £Jjj| 


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20 

21 

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23 

24 

25 

26* 

27 

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HES 1 

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41 

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46 

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43 

50 

51 

52 1 

53 

54 

55 

56 


ZONE | SYM | 


REVIS.ONS TD ft ft Ot76~5 _ 

| DATE | APPftOV/U- 


OESCRIPTION 



REQUIREMENTS 

1. general; 

A. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS 
~ 7 . .SPECIFIED IN ND1015404 CLASS 3 

C. IDENTIFY USING DRAWING NUMBER, APPLICABLE DASH NO. , REVISION 

LETTER $ MANUFACTURERS SYMBOv. PER MIL-STD-I30. MANUFACTURERS. 
77 NAME AND PART NO. MAY ALSO BE USED. 

70. UNLESS OTHERWISE SPECIFIED SCREWS MUST MEET REQUIREMENTS 
^ OF FF-S-86 TYPE VL 

2 . INSPECTION £ ACCEPTANCE. 

A. MATERIAL.* 410 CRES PER MIL-5-S62 CLASS 3 

b^finish; passiwte per mil-f-i+072 fin e-3oc 
i-A31 


PROCURE ONLY FROM APPROVED SOURCES 
.LISTED IN NDI002.034 FOR THIS DRAWING 


& 

fKMtt 




QTY. 

I REQO. 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


LIST OF PARTS AND MATERIALS 


•‘ft 


• • 

• • • • 
• • • 


MULTIPLE 


USAGE 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


M I T 

INSTRUMENTATION LAS 

CONTRACT 

NAS 9153 I 


DO NOT SCALE THIS DRAWING 



_ SCREW.... __ 

~~~ HE* SOC HD 
SPECIF ICATfON CONTROL. DWG 


SCALE 


UNIT WT. 


COOE IDENT. 


MIT 

INSTRUMENTATION | 

LABORATORY 

Cammidm, Mam. 

. 

OWQ. NO. 

r 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING Na 


~ 1001489~~ 

SHEET 1 OF | 



„ . K i 

& ' l 

it 

Lw weiti i , 

s 1 










INCHES 

I a J i i 1.J I 

O I £ 


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6 


_°_l_:_-j--- 

RBJUIRBCXTS: 

1. GENERAL: 

A. INTERPRET DRAWING IN ACCORDANCE WITN STANDARDS PRESCRIBED IN MIL-D-70327. 

B. SUPPLIERS SMALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN NO 1015404, CLASS 2, 

C. UNITS SMALL BE CAPABLE OF MEETIN6 ALL QUALIFICATION REQUIREMENTS SPECIFIED IN NO 1002052. 

B. UNITS SMALL MEET THE MATERIAL ANO PERFORMANCE REQUIREMENTS OF MIL-C-2G482. TYPE NS 5114H-10- 2P. 

EXCEPT FOR SHELL PLATING. 

I. MRKIM6: UNITS MO SNIPPING CONTAINERS SHALL OE T ^ Y 

NASA DRAWING NUMBER, DASH NUMBER ANO REVISION LETTER. THE MANUFACTURER S PART NUMBER MAY APPEAR 

. ON THE UNIT OR CONTAINER. 

F. UNIT SMALL BE SUPPLIED WITH PROTECTIVE COVER NASA DRAWING NUMBER 1001495. 

2. INSPECTION AND ACCEPTANCE: 

A. DIMENSIONS: AS SHOWN 

B. DIELECTRIC WITHSTANDING V0LTA6E (SEA LEVEL): 1500 VOLTS, RMS 

C. INSULATION RESISTANCE: 5,000 MEGOHMS MINIMUM AT 500 VDC 


5. DESIGN REQUIREMENTS: 

A. CONNECTOR: RECEPTACLE, SOLDER TERMINALS, REAR N0UNTIN6 WITH NUT, BAYONET COUPLING, HERMETICALLY 
SEALED, PIN CONTACTS. 

B. OPERATING TEMPERATURE: *125*C 

C. CURRENT RATING: 5 AMPERES 

B. V0LTA6E RATING: 500 VOLTS RMS OR 700 VOLTS DC 
E. DIELECTRIC WITHSTANDING VOLTAGE (70,000 FEET): 375 VOLTS, RMS 

f'. SHELL: SHALL BE PER MIL-C-24402 EXCEPT THE PLATING SHALL BE TIN OVER COPPER PLATIN6. 

B. CONTACTS: 32 PIN CONTACTS; 120 SIZE 
N. POLARIZATION: PER TABU I 

4. CONTACT RESISTANCE: 70 MILLIVOLTS, MAXIMUM AT 5 AMPERES 

K. CONTACT MATERIAL: TIN PLATIN6 OVER NICKEL ALLOY MATERIAL 

L. O'RING MATERIAL: EXTERNAL PACKING: NEOPRENE RUBBER PER MS29513-2B 

INTERNAL PACKING: SILICONE RUBBER 


> PROCURE ONLY FROM APPROVED SOURCES LISTED IN ND1002034 FOR THIS DRAWING 
TABLE! 



1004492-1 1001492-2 1001492-3 100*492-4 


6 









































































ZONE I SYM 


DESCRIPTION 


DATE 


APPROVAL 



NOTES 

. L INTERPRET: DRAWING IN /MXORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

L INDEWTIFY USING DRAWING NO*' REVISION LETTER AND 
1 NV\NUEACTURERS... SYMBOL PER NUL-STD-J30 . WIANUFACTURERS 
~ NUMBER AND NAME MAY ALSO BE USED . 

3. ITEM MUST _MATE_ .WITH jCONNECTOR AIASA DWG A/OZIOOI492 

4, MATL, __ 

body: aluminum; die cast AMS4iae 

CHAINi STAINLESS STEEL PASSIVATED 

DISK! SYNTHETIC RUBBER MlL-STD-417 SE*I 0 DUROMETER 


SS* -'■ —''■ 


PROCURE ONLY FROM APPROVED SOURCES 1~ 
LISTED IN ND1002034 FOR THIS DRAWING 


<?ty 

reqo. 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL FIND 

OR NOTES NO. 


1 



UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOtERANCES ON 



FRACTIONS DECIMALS ANGLES 





DL100/500 

DO NOT SCALE THIS DRAWING 


DLI00020I 

MATERIAL: 

SEE NOTE 4 : : Z j: s 

NEXT ASSY 

USED ON 

APPIIC 

xm 



M I T 

INVntUMKNTATtOH I 


NAS 9153 I 




BLACK M-*a-fe3l 


MSC 


MIT/l^ APPROVAL 


\nM 


w 


INCHES ,, 

1 ■ 1 • I ■ 1 ‘ I 
0 12 
PHOTOGRAPHIC SCALE ONUT 




LIST OF PARTS AND MATERIALS 


cover: 

PROTECTIVE . 

1 —vrrr -- 

INSTRUMENT ATION 
LABORATORY 

CA1MMHMMC. MASBi 

ELECTRICAL CONNECTOR 

ONI. MO. 

•SPECIFICATION CONTROL DRAWING 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 




NASA DRAWING NO. 

SCALE 

2/1 

UNIT WT. 

CODE IDENT. 

1001495 _ 



SHEET OF 


I 




















































REQUIREMENTS: 


IT OTHKR PC MON ON CORPORATION. ON CONVtT. 

MUON TO NANUFACTURC. NSC. ON SCU. AM 

T IN ANT WAT SI Nf LATIN TNBMTO. 


ronn- ots ~2.it- 


1. GENERAL: 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BT MIL-D-70327. 

B. UNITS SHALL BE CAPABLE OF MEETING THE REQUIREMENTS OF NtL-C-8384, EXCEPT AS 
AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

C. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN 
NO 1015404, CLASS 2. 

D. UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED 
IN ND 1002052 UNLESS MODIFIED OR AMMENDEO BY THE DESIGN REQUIREMENTS 
SECTION (3) OF THIS DRAWING. 

E. PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001497), REVISION LETTER. DASH NUMBER (IF ANY), 

THE MANUFACTURER’S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING 
DATE OR CODE. 

F. MARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001497), REVISION LETTER, 

AND DASH NUMBER (IF ANY) SHALL BE MARKED ON THE PART PER M1L-STD-130. 

2. ■ ACCEPTANCE AND INSPECTION 

A. DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 750 VOLTS, RMS HlN* 

B. INSULATION RESISTANCE: ZOOK MEGOHMS, MINIMUM AT 500 VOLTS DC. 

3. DESIGN REQUIREMENTS: 

A. MAXIMUM WORKING VOLTAGE: 250 VOLTS DC. 

DIELECTRIC WITHSTANDING VOLTAGE; 100,000 FEET: 500 VOLTS,RMS. 

C. CURRENT RATING: 3 AMPERES RMS, MINIMUM. 

D. CONTACT VOLTAGE DROP: 25 MILLIVOLTS, MAXIMUM AT 3 AMPERES DC. 

£. INSERTION AND WITHDRAWAL FORCE (WITH MATING CONNECTOR): 2 OUNCES MIMIMUM- 
4 OUNCES MAXIMUM, PER CONTACT. 

F. CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT, THE CONTACT 

VOLTAGE DROP AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 

6. DIELECTRIC MATERIAL: DIAU.VL PHTHALATE, GLASS FILLED PER MIL-M-14, TYPE SDG. 

H. LEADS: SHALL BE #28 STRANOED LEADS. TEFLON INSULATED, PER MIL-W-1M78, 

TYPE ET, COLOR CODED PER TABLE l. 

I. CAPTIVE SCREW: #2-56NC-2A CAPTIVE SCREW; STEEL, WITH A CADMIUM PLATE. 

J. MOUNTING PLATE: BRASS, WITH FUSED ELECTRO-TIN ON CADMIUM PLATE OVER COPPER FLASH. 

K. STUD: I2-5GNC-2B TAPPED STUD; STEEL, WITH FUSED ELECTRO-TIN ON CADMIUM PLATE OVER COPPER FLASH. 
INTERNAL THREADS TO BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENEO SECURELY AND 
HERMETICALLY SEALED TO MOUNTING PLATE. 

L. VIBRATION: DURING VIBRATION PER ND 1015404, DISCONTINUITY SHALL BE 1 MICROSECOND OR LESS. 


PROCURE ONLY FROM APPROVED SOURCES LISTED IN 
NO 1002034 FOR THIS DRAWING. 



QTY PART OR NOMENCLATURE OR FIND 

REQO IDENTIFYING NO. DESCRIPTION NO. 

LIST OF MATERIALS 



UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 

TOLERANCES ON 

M 1 T 

INSTRUMENTATION LAB 
Cammidm. Mam. 

RWR. MO. CONTRACT 

MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS x 





FRACTIONS DECIMALS ANGLES 

± — ± — ± — 

DO NOT SCALE THIS DRAWING 

DRAWN TV/rtfO DATE^-*'-**' 

CHECKEO W )A/flFPf._ 

APPROVAL £ 

C0MA/£Cr0&, & fC7}e/C>U 
?£■ co#rAcrs, />u/e £ ttcrmcis 

jssc/s/ca r/&// co/rrsoi /?****/#& 

_ 





MATERIAL 

Js X//0PYA/ 

ipconun 






HEAT TREATMENT 

FINAL FINISH 

NASA APPTOVAL^tt^f-T? TA. ^ 

MIT APPROVAI^C-ujt/TXijM^f 

^OOE IDENT NO. 

SIZE 

C 

NASA DRAWING NO. 

1001497 

NEXT ASSY 

USED ON 

| APPLICATION 

SCALE — 

WT | SHEET / OF 2 






























































































3 


2 



A61?I00I 


REQUIREMENTS; 
1. GENERAL: 


-,-" tvt,,ON « -rr>* £0i2Si 

_ pocmmoH _ PAT« AInwm 

A A 00&0 j wevr /, /rfr/sw z r-i-i3 t I 

0AVAA000 T0 ciass a -OA* fa 

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A/ ser/f/o// srA/T/s scoc* ^-4-ii FAT I 

R REPLACED BY REV C „/. t 

B PER TDRR IPllH lUM tpr 


A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. UNITS SHALL BE CAPABLE OF MEETING THE REQUIREMENTS OF NIL-C-8384, EXCEPT AS 
AND IN ADDITION.TO THE REQUIREMENTS SPECIFIED HEREIN. 

C. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN 
ND 1015404, CUSS 2. 

D. UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED 
IN ND 1002052 UNLESS MODIFIED OR AMMENDED BY THE DESIGN,REQUIREMENTS 
SECTION (3) OF.THIS DRAWING. 

E. PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001497). REVISION LETTER, DASH NUMBER (IF ANY). 

THE MANUFACTURER’S NAME OR SYMBOL,.LOT OR SERIAL NUMBER AND THE MANUFACTURING 
DATE OR CODE. 

F. NARKING: THE MANUFACTURER’S NAME OR SYMBOL, DRAWING NUMBER (1001497), REVISION LETTER, 

AND DASH NUMBER.(IF ANY) SHALL BE MARKED ON THE PART PER MIL-STD-130. 

2. - ACCEPTANCE AND INSPECTION \ 

A. DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 750 VOLTS, RMS tfW* 

B. INSULATION RESISTANCE: 200K MEGOHMS, MINIMUM AT 500 VOLTS DC. 

3. DESIGN REQUIREMENTS: 

A. MAXIMUM WORKING VOLTAGE: 250 VOLTS DC. 

.B. OIGLECTRIC WITHSTANDING VOLTAGE; 100,000 FEET: 500 VOLTS.RMS. 

C. CURRENT RATING: 3 AMPERES RMS, MINIMUM. 

0. CONTACT VOLTAGE DROP: 25 MILLIVOLTS, MAXIMUM AT 3 AMPERES DC. 

C. INSERTION AND WITHDRAWAL FORCE (WITH MATING CONNECTOR): 2 OUNCES MINIMUM- 
4 OUNCES MAXIMUM, PER CONTACT. 

F. CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT, THE CONTACT 
VOLTAGE DROP AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 

G. DIELECTRIC MATERIAL: DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-14, TYPE SDG. 

H. LEADS: SHALL BE 128 STRANDED LEADS, TEFLON INSULATED, PER MIL-W-1G878. 

TYPE ET, COLOR CODED PER TABLE X. 

I. CAPTIVE SCREW: I2-5GNC-2A CAPTIVE SCREW; STEEL, WITH A CADMIUM PLATE. 

J. MOUNTING PUTE: BRASS, WITH FUSED ELECTRO-TIN ON CADMIUM PLATE OVER COPPER FLASH. 

K. STUD: I2-5GNC-2B TAPPED STUD; STEEL. WITH FUSED ELECTRO-TIN ON CADMIUM PUTE OVER COPPER FUSH. 
INTERNAL THREADS TO BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENED SECURELY AND 
HERMETICALLY SEALED TO MOUNTING PUTE. 

L. VIBRATION: DURING VIBRATION PER NO 1015404, DISCONTINUITY SHALL BE 1 MICROSECOND OR LESS. 


©REPLACED BY REV C WITH CHANGES 


Xtvnrr , \X¥£-4rr 2 

5-7xt(/s 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


PROCURE ONLY FROM APPROVED SOURCES LISTED IN 
NO 1002034 FOR THIS DRAWING. 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

* ~ ± — ± — 

DO NOT SCALE THIS DRAWING 
MATERIAL — 

S/VOPYA/ 


M I T 

INSTRUMENTATION LAS 


CHECKED. 

APPROVAL 

APPROVAL. 



LIST OF MATERIALS _ 

MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 

COMA/£Cr0&, &£C£se/C*i 
zs* cwrAcrs, /%</* £ x&csrrAct £ 

S/>£7C//r/cA r/0Af CO/Y/rod. 


NEXT ASSY 


USED ON 


I HEAT TREATMENT 


I FINAL FINISH 


I NASA APPROVAL^ 


CODE IDENT NO. I SIZE 


APPLICATION 




1 MIT APPROVi 




NASA DRAWING NO. 

100(497 





n 






































.1 _. 



NOTICE — WHEN aOVERNMCNT WAWINM. SPECIPICATIOIIt. M OTHER DATA 
ARC USED TOR ART PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
BELATED COVERNNENT PROCUREHENT OPERATION. THE UNITED STATES GOVERN¬ 
MENT THEREBY INCURS NO RESPONSIBILITY NOR ANY OBLIGATION WHATSOEVER; 
ABO THE FACT THAT THE GOVERNMENT MAY HAVE FORMULATED. FURNISHEO. OB 
IN ANY WAY SUPPLIED THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO BE REGARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSING THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY¬ 
ING ANY RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL AMY 
PATENTED INVENTION THAT NAT IN ANT WAY BE RCLATCO THERETO. 



REVISIONS 


DESCRIPTION 


REPLACES SHEET I REV B 


I WITH CHANGES IQg? 


■- w 

0 unfl 


REQUIREMENTS: 


GENERAL 


INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

UNITS SHALL BE CAPABLE OF MEETING THE REQUIREMENTS OF MIL-C-8384. EXCEPT AS 
AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN NO 1015404, CLASS 2. 
UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED*IN NO 1002052 
UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS SECTION (3) OF THIS DRAWING. 
.PACKAGING AND PACKING:UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001491). REVISION LETTER, DASH NUMBER f “ 

THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING DATE 
OR CODE. UNITS SHALL BE INDIVIDUALLY PACKAGED PER ND 1002215, CLASS I 
MARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001491), REVISION 
LETTER AND DASH NUMBER SHALL BE MARKED ON THE UNIT PER ND 1002019. 


ACCEPTANCE AND INSPECTION 


DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 900 VOLTS RMS MINIMUM PER METHOD 301 OF M3L-STD-202 

INSULATION RESISTANCE: 200K MEGOHMS, MINIMUM AT 500 VOLTS DC PER METHOD 302 OF MIL-STD-202. 
DIMENSIONS AS SPECIFIED HEREIN. 

100% INSPECTION: INSPECT OPTICALLY FOR EVIDENCE OF CRACKS, BURRS, LOOSE CONTACTS, 

CONTACT ALIGNMENT. VOIDS,FLAWS OR ANY FOREIGN MATTEL DETRIMENTAL TO THE FUNCTION OF 
THE CONNECTOR. CONTACT MATING SURFACES SHALL BE FREE FROM CRACKS, BURRS, BENDS AND 
FOREIGN PARTICLES. 


DESIGN REQUIREMENTS: 

MAXIMUM WORKING VOLTAGE: 250 VOLTS DC, 175 VOLTS RMS. 

DIELECTRIC WITHSTANDING VOLTAGE: 100,000 FEET: 250 VOLTS RMS. PER METHOD 301 OF MIL-STD-202 
CURRENT RATING: 3 AMPERES RMS MINIMUM 

CONTACT VOLTAGE DROP: 25 MILLIVOLTS, MAXIMUM AT 3 AMPERES DC. 

INSERTION AND WITHDRAWAL: (WITH MATING CONNECTOR) INDIVIDUAL CONTACTS SHALL 
HAVE A MAXIMUM ENGAGEMENT FORCE OF 6 OUNCES AND A MINIMUM WITHDRAWAL FORCE OF 
.5 OUNCES. ASSEMBLIES SHALL NOT EXCEED A MATING FORCE IQUAL TO THE PRODUCT OF 
THE NUMBER OF CONTACTS X 7.5 OUNCES OR A WITHDRAWAL FORCE EQUAL TO THE PRODUCT 
OF THE NUMBER OF CONTACTS X 1 OUNCE. 

CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT OF THE CONNECTOR AT 120 CYCLES/HOUR MAX. 
THE CONTACT VOLTAGE DROP AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 

DIELECTRIC MATERIAL: (BODY) DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-19833, GDI-30- 
LEADS: SHALL BE 28 STRANDED WIRE, TEFLON INSULATED, PER-*1L-W-16878. TYPE ET, 

COLOR COOED PER TABLE I. i 

(1) LEADS SHALL WITHSTAND A 4 LB AXIAL P$LL(APPLIED GRADUALLY)FOR 10 SECONDS. I 

CAPTIVE SCREW: CRES TYPE 303 PER MIL-S-7720, PASSIVATED PER FINISH 5.4.2 OF MIL-STD-171 

MOUNTING PLATE: BRASS. TIN PLATED PER MIL-T-10727, TYPE I OVER COPPER FLASH. 

STUD: STEEL, TIN PLATED PER MIL-T-10727, TYPE I OVER COPPER FLASH. INTERNAL THREADS TO 
BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENED SECURELY AND HERMETICALLY SEALED 

TO MOUNTING PLATE. .-,-,- 


©REPLACES SHEET I REV B WITH CHANGES 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


UST OF MATERIALS 


.PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND 1002034 FOR THIS DRAWING 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES ,N 

TOLERANCES ON ow m 

FRACTIONS DECIMALS ANGLES 0RA *N 


M I T 

INSTRUMENTATION LAB 


MANNED SPACECRAFT CENTER 


Cammiow, Maw. 


HOUSTON, TEXAS 


CHECKED 


DATE 7-/~^ 
4 7-/-<» 


DO NOT SCALE THIS DRAWING 
MATERIAL 


CONNECTOR. ELECTRICAL 

25 CONTACTS, PLUG £ RECEPTACLE 


AS SHOWN 


I HEAT TREATMENT 


NASA APPROVAL 


SPECIFICATION CONTROL DRAWINC 

CODE IDENT NO. I SIZE I NASA DRAWING NO. 


I FINAL FINISH 


1001497 


APPLICATION 


AS SHOWN 


MIT APPROVAL 


I SHEET | OF 3 


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3 


2 



NOTICE - WHKN SOVERNMCNT DRAWINGS. SPCC1FICAYIONS. OH OTHER DATA 
ARE USED FOR ARY FURFOSE OTHER THAR IN CONNECTION WITH A DEFINITELY 
RELATED DOVERNMENT PROCUREMENT OPERATION. THE UNITED STATES COVERN- 
MENT THERERY INCURS NO RESFONSIRIUTY NOR ANY ORLI6ATION WHATSOEVER: 
AMO THE FACT THAT THE COVERNMEHT MAY HAVE FORMULATEO. IURNISHEO. OR 
IN ANY WAY SUPPLIED THE SAID DRAWINSS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO RE RECARDED RY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSINC THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY- 
INC ANY RICHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL ANY 
PATENTED INVENTION THAT NAY IN ANY WAY RE RELATEO THERETO. 


L. VIBRATION: DURING VIBRATION PER 1002052, DISCONTI NUN ITY SHALL BE 0-1 MICROSECOND 
OR LESS. AT 100 MA DC FOR MATED CONNECTORS. 

M. CONTACT RESISTANCE: 10 MILL I OHMS MAX AT 100 MADC TEST PER MIL-STD-202, METHOD 307. (MATED.PAIRS) 

N. TEMPERATURE OPERATING: -55°C TO +150 # C. 


_ REVISIONS 

DESCRIPTION 


jpyy 

I DATE I APPROVAL. 


THIS SHEET ADDED t0 97 < 


MW- 


SPECIAL REQUIREMENTS: (BY SUPPLIER) 

CONTACT SEPARATION: (100* INSPECTION) ALL PIN CONTACTS SHALL BE TESTED WITH A 

STEEL TEST SLEEVE HAVING AN INSIDE DIAMETER OF .0230 +0001 AND FINISH OF 16 

-0000 

MICRO-INCHES MAX. THE TOTAL WEIGHT OF THE TEST SLEEVE SHALL BE .5 OUNCES +.1 

-.0 

WHEN THE ASSEMBLY IS INVERTED THE PIN CONTACT SHALL RETAIN THE .5 OUNCE WEIGHT. 

THIS TEST SHALL BE PERFORMED ON THE CONTACTS PRIOR TO ASSEMBLY WITH THE CONNECTOR BODY. 
THE FOLLOWING LOT SAMPLE TESTS SHALL BE MADE PPIOR TO 
shipment: . 

(1) TENSILE STRENGTH: 

THE CRIMPED ASSEMBLIES FROM EACH TOOL SHALL BE SAMPLED PER MIL-STD-414 
INSPECTION LEVEL IV, AQL .4. THE ASSEMBLIES SHALL BE TESTED ON A HUNTER SCALE 

FOR TENSILE STRENGTH AND THE READINGS SHALL BE RECORDED. ALL ASSEMBLIES 
SHALL BE WITHIN THE CONTROL LIMITS STATED BELOW OR THE LOT SHALL BE 

REJECTED. ASSEMBLIES SHALL BE PACKAGED AND IDENTIFIED WITH THE LOT NUMBER, 

WHICH SHALL ACCOMPANY THE UNITS TO FINAL INSPECTION, AND BE INCLUDED WITH 
THE CONNECTOR SHIPMENT. THIS APPLIES TO BOTH PINS AND SOCKETS. 

THERE SHALL BE TWO DATA SHEETS FOR THE CRIMPING OF THE PINS, ONE FOR THE PIN END 
AND ONE FOR THE WIRE END. 


\l 



PIN 


SOCKET 

WIRE 

CONTACT 

WIRE 

WIRE 

SIZE 

END (MIN) 

EN0 (MIN) 

END (MIN 

28 

3.0 LBS 

4.0 LBS 

4.0 LBS 


( 2 ) SOCKET STRENGTH, SIDE LOAD (IN CONNECTOR): 18 
THE PIN ENGAGING END OF THE SOCKET. INTERMATABILIT 


8 OUNCES MINIMUM SHALL BE APPLIED AT 
TY AND PERFORMANCE SHALL NOT BE 


IMPAIRED. 


C MATING AND CLEANING: (100% INSPECTION) EACH CONNECTOR SHALL BE MATED 5 TIMES AND T^EN 

ULTRASONICALLY CLEANED FOR 1/2 MINUTE. INSPECT FOR LOOSE, CRUSHED OR MISALIGNMENT ’ 

OF CONTACTS. 


© THIS SHEET ADDED 


NEXT ASSY 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
± ± ± 

DO NOT SCALE THIS DRAWING 
MATERIAL 

AS SHOWN 

HEAT TREATMENT 

FINAL FINISH 

AS SHOWN 


PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAB 
Cammiom. Mam. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


DRAWN rj, CUUL 
CHECKED -QLh 

approvai^LSvJ 

APPROVAL jQUt 
NASA APPROVAL. 

7 

MIT APPROVAL 


E *£g CONNECTOR. ELECTRICAL 

25 CONTACTS.PLUG £ RECEPTACLE 

_ SPECIFICATION CONTROL DRAWING 

S CODE IDENT NO. I SIZE I NASA DRAWING NO. 

c 1001497 

SCALE fwT |SHEET 2 Of 5 



















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REVISIONS 


NOTICE — WHEN ROVERNNCNT QRAWINRR. RPfCIFICATIONS. OR OTHER DATA 
ARE USED FOR ANT PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
RELATED GOVERNMENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN¬ 
MENT THERERT INCURS NO RESPONSIRILITY NOR ANT ORLIGATION WHATSOEVER; 
AMO THE FACT THAT THE GOVERNMENT NAT HAVE FORMULATED. FURNISHED. OR 
IN ANT WAT SUPPLIED THE S*IO DRAWINGS. SPECIFICATIONS OR OTHER DATA It 
NOT TO RE REGARDED »Y IN. 'CATION OR OTHERWISE AS IN ANT MANNER 
LICENSING THE HOLDER OR ANT OTHER PERSON OR CORPORATION. OR CONVEY¬ 
ING ANT RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL ANY 
PATENTED INVENTION THAT MAT IN ANY WAY RE RELATED THERETO. 


REQUIREMENTS: 


I.’. 

A. 

• 

C. 

D. 

E. 


F. 


GENERAL 


INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

UNITS SHALL BE CAPABLE OF MEETING THE APPLICABLE REQUIREMENTS OF MIL-C-8384. 

AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. , . _ 

SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND 1015404 


EXCEPT AS 


CLASS 2. 


UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED IN ND 1002052 
UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS SECTION (3) OF THIS DRAWING. 
PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001497). REVISION LETTER, DASH NUMBER 
THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING DATE 
OR CODE. UNITS SHALL BE INDIVIDUALLY PACKAGED PER ND 1002215, CLASS I 
MARKING: THE MANUFACTURER'S NAME OR SYMBOL. DRAWING NUMBER (1001497). REVISION 
LETTER AND DASH NUMBER ??*) SHALL BE MARKED ON THE UNIT PER ND 1002019. 


2.. ACCEPTANCE AND INSPECTION 


A. DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 900 VOLTS RMS MINIMUM PER METHOD 301 OF M(lL—STD-202 

B. INSULATION RESISTANCE: 200K MEGOHMS. MINIMUM AT 500 VOLTS DC PER METHOD 302 OF MIL-STD-202. 

C. DIMENSIONS AS SPECIFIED HEREIN. 

D. 100* INSPECTION: INSPECT OPTICALLY FOR EVIDENCE OF CRACKS. BURRS. LOOSE CONTACTS. 

CONTACT ALIGNMENT, VOIDS,FLAWS OR ANY FOREIGN MATTER DETRIMENTAL TO THE FUNCTION OF 
THE CONNECTOR. CONTACT MATING SURFACES SHALL BE FREE FROM CRACKS, BURRS, BENDS AND 
FOREIGN PARTICLES. 



3. 


F. 


DESIGN REQUIREMENTS: 

MAXIMUM WORKING VOLTAGE: 250 VOLTS DC, 175 VOLTS RMS. 

DIELECTRIC WITHSTANDING VOLTAGE: 100,0OO FEET: 250 VOLTS RMS. PER METHOD 301 OF MIL-STD-202 
CURRENT RATING: 3 AMPERES RMS MAXIMUM 

CONTACT VOLTAGE DROP: 25 MILL'IVOLIS, MAXIMUM AT 3 AMPERES DC. 

INSERTION AND WITHDRAWAL: (WITH MATING CONNECTOR) INDIVIDUAL CONTACTS SHALL 
HAVE A MAXIMUM ENGAGEMENT FORCE OF 6 OUNCES AND A MINIMUM WITHDRAWAL FORCE OF 
.5 OUNCES. ASSEMBLIES SHALL NOT EXCEED A MATING FORCE EQUAL TO THE PRODUCT OF 

THE NUMBER OF CONTACTS X 7.5 OUNCES OR BE LESS THAN A MINIMUM WITHDRAWAL FORCE EQUAL TO THE PRODUCT 
OF THE UJMBER OF CONTACTS X 1 OUNCE. 

CONTACT LIFE- AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT OF THE CONNECTOR AT 120 CYCLES/HOUR MAX. 
THE CONTACT VOLTAGE DROP SHALL BE 35 MV AT 3 ADC AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN 
DIELECTRIC MATERIAL: (BODY) DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-19833, GDI-38. 

LEADS: SHALL BE 28 STRANDED WIRE. TEFLON INSULATED, PER-*IL-W-16878. TYPE ET, 

COLOR COOED PER TABLE I. 

(1) LEADS SHALL WITHSTAND A 4 LB AXIAL PflLL(APPLIED GRADUALLY)FOR 10 SECONDS. 

CAPTIVE SCREW: CRES TYPE 303 PER MIL-S-7720, PASSIVATED PER FINISH 5.4.2 OF MIL-STD-171 

MOUNTING PLATE: BRASS, TIN PLATED PER MIL-T-10727, TYPE I , FUSED OVER COPPER FLASH. 

STUD: STEEL, TIN PLATED PER MIL-T-10727, TYPE I , FUSED OVER COPPER FLASH. INTERNAL THREADS TO 
BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENED SECURELY AND HERMETICALLY SEALED 
TO MOUNTING PLATE. 


©REPLACES SHEET I REV B WITH CHANGES 


i 


► 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND 1002034 FOR THIS DRAWING 
















NEXT ASSY 

USED ON 

j APPLICATION | 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FACTIONS DECIMALS ANGLES 
±: db — 


DO NOT SCALE THIS DRAWING 


MATERIAL 

AS SHOWN 


HEAT TREATMENT 


FINAL FINISH 

AS SHOWN 


QTY 

REQD 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


FIND 

NO. 


LIST OF MATERIALS 


MIT 

INSTRUMENTATION LAS 


Cambiums. Mam. 

CONTRACT 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


DRAWN < 7 jl DATE 7-/-*^ 

CHECKED 7 - 1 - 6 * 

A 

APPROVAL 


APPROVAL 


NASA APPROVAI 


MIT APPROVAL 



CONNECTOR, ELECTRICAL 

25 CONTACTS, PLUG < RECEPTACLE 

SPECIFICATION CONTROL DRAWING 


CODE IDENT NO. 


SCALE 


SIZE 


NASA DRAWING NO. 


WT 


1001497 

[sheet I of 3 


INCHES 

l.i l 


0 I 

•MH0T06RAPH1C SCALE 


"-H- 1* 

SALE OfUT J 













APPROVAL 


NOTICE 
ARC USED FOR 
RELATED GOVERNMENT 
RENT THERERVINCURS 


DRAWINGS. SPECIFICATIONS. OR OTHER DATA 
IN CONNECTION WITH A DEFINITELY 
E UNITED STATES GOVERN- 
OGLICATION WHATSOEVER; 

SHED. OR 


a z6t?iooi 


NtVI»IUN3 

DESCRIPTION 




MFLICATION OR OTHERWISE AS IN ANT MANNER 
OTHER PERSON OR CORPORATION. OR CONVEY- 
NANUFACTURE. USE. OR SELL AMY 
RE RELATED THERETO. 


C THIS SHEET ADDED \oi 74 
D REVISED PER TDRR 11142 




L. VIBRATION: DURING VIBRATION PER NO 1002052, 01SC0NTINUNITY SHALL BE o.l MICROSECOND 

OR LESS. AT 100 MA DC FOR MATEO CONNECTORS. - oa.dcT 

A. CONTACT RESISTANCE: 10 MILL I OHMS MAX AT 100 MADC TEST PER MIL-STD-202, METHOD 307. (MATED— PAIRS l 

H. TEMPERATURE OPERATING: -55 # C TO +150°C. 


SPECIAL REQUIREMENTS: (BY SUPPLIER) 

A. CONTACT SEPARATION: (100% INSPECTION) ALL PIN CONTACTS SHALL BE TESTED WITH A 
STEEL TEST SLEEVE HAVING AN INSIDE DIAMETER OF .0230 ♦OOOIj AND FINISH OF Ifc 
MICRO-INCHES MAX. THE TOTAL WEIGHT OF THE TEST SLEEVE SHALL BE .5 OUNCES + J 

WHEN THE ASSEMBLY IS INVERTED THE PIN CONTACT SHALL RETAIN THE .5 OUNCE WEIGHT. 

THIS TEST SHALL BE PERFORMED SEQUENTIALLY ON EACH CONTACT AFTER ASSEMBLY WITH THE CONNECTOR BODY. 

B. THE FOLLOWING LOT SAMPLE TESTS SHALL .BE MADE PPIOR TO 
shipment: 

(1) Se S crimped E assemblies from each tool shall be sampled PER MIL-STD-414 

INSPECTION LEVEL IV. AQL .4. THE ASSEMBLIES SHALL BE TESTED ON A HUNTER SCALE (OR EQUIVALENT) 

FOR TENSILE STRENGTH AND THE READINGS SHALL BE RECORDED. ALL ASSEMBLIES 
'SHALLBEWITHINTHE CONTROL LIMITS STATED BELOW OR THE LOT SHALL BE 

REJECTED. ASSEMBLIES SHALL BE PACKAGED AND IDENTIFIED WITH THE LOT NUMBER, 

WHICH SHALL ACCOMPANY THE UNITS TO FINAL INSPECTION, AND BE INCLUDED WITH 
THE CONNECTOR SHIPMENT. THIS APPLIES TO BOTH PINS AND SOCKETS. 

THERE SHALL BE TWO DATA SHEETS FOR THE CRIMPING OF THE PINS, ONE FOR THE PIN END 
AND ONE FOR THE WIRE END. 


SOCKET 

WIRE CONTACT WIRE WIRE 

SIZE END (min) _ END (MIN) _ END (MIN) 

28 3.0 LBS ” 4.0 LBS _ 4.0 LBS 

f?)SOCKET STRENGTH, SIDE LOAD (IN CONNECTOR): 18 OUNCES MINIMUM SHALL BE APPLIED AT 
'■THE PIN ENGAGING END OF THE SOCKET. INTERMATABILITY AND PERFORMANCE SHALL NOT BE 

IMPAIRED. 

C MATING AND CLEANING: (100% INSPECTION) EACH CONNECTOR SHALL BE MATED 5 TIMES AND ThEN 
ULTRASON ICALLY CLEANED FOR 1/2 MINUTE. INSPECT FOR LOOSE, CRUSHED OR MISALIGNMENT 
OF CONTACTS. 


© THIS SHEET ADDED 


UNLESS OTHERWISE SPECIFIED 

INS1 

DIMENSIONS ARE IN INCHES 

TOLERANCES ON »»• "> _ 

FRACTIONS DECIMALS ANGLES DRAWN & 

zt ± ±i 

CHECKED 

DO NOT SCALE THIS DRAWING APPROVAL 

MATERIAL APPROVAL. 

AS SHOWN 

HEAT TREATMENT AOI 


PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAB 
Cambiums. Mam. 

. NO. _COMTBACV_ 


NOMENCLATURE OR 
DESCRIPTION 

LIST OF MATERIALS __ 

MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


APPLICATION 


USED ON final FINISH 

4 AS SHOWN 


CONNECTOR, ELECTRICAL 

25 CONTACTS.,FLUG £ RECEPTACLE 


SPEC IF1CAT10N CONTROL DRAWING 


NASA APPROVAL. 


MIT APPROVAL 1 


CODE IDENT NO. SIZE 


NASA DRAWING NO. 

1001497 


SHEET Z OF 3 


iU 


INCHES 


0 I ' Z" 

photographic scale ONLY j 
























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—/ _ 00002X0220 00AAA20 

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PART OR 
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UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 


M I T 

INSTRUMENTATION LAS 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS _ 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


coASA/£~cro/?, fiFcr&c/u 

2S CO/V7XCT5, 

SSFC/ZVCAr/OAS <ro//r*0£ J>A4PV///*r 




NASA DRAWING NO. 

1001497 
















































ICE — WHEN GOVERNMENT DRAWINGS. SPECIFICATIONS. OR OTHER DATA 
USED FOR ANY PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
TED GOVERNMENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN- 
THEREGY INCURS NO RESPONSIBILITY NOR ANY OBLIGATION WHATSOEVER: 
THE FACT THAT THE GOVERNMENT MAY HAVE FORMULATED. FURNISHED. OR 
ANY WAV SUPPLIED THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
: REGARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY- 
RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL ANY 
NVENTIOM THAT MAY IN ANY WAY BE RELATED THERETO. 


Z6W00I 


REQUIREMENTS: 

, . GENERAL 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY Mll-D-70327. 

B. UNITS SHALL BE CAPABLE OF MEETING THE APPLICABLE REQUIREMENTS OF MIL-C-8384. EXCEPT AS 
AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

C. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND 1015404, CLASS 2. 

D. UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED IN ND 1002052 
UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS SECTION (3) OF THIS DRAWING. 

E. .PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001491). REVISION LETTER, DASH NUMBER ' 

THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING DATE 
OR CODE. UNITS SHALL BE INDIVIDUALLY PACKAGED PER ND 1002215, CLASS I 

F. MARKING: THE MANUFACTURER’S NAME OR SYMBOL, DRAWING NUMBER (1001491), REVISION 
LETTER AND DASH NUMBER ~ SHALL BE MARKED ON THE UNIT PER ND 1002019. 


ACCEPTANCE AND INSPECTION 

A. DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 900 VOLTS RMS MINIMUM PER METHOD 301 OF MIL-STD-202 

B. INSULATION RESISTANCE: 200K MEGOHMS, MINIMUM AT 500 VOLTS DC PER METHOD 302 OF MIL-STD-202. 

C. DIMENSIONS AS SPECIFIED HEREIN. 

D. 100% INSPECTION: INSPECT OPTICALLY 10 X MAGNIFICATION FOR EVIDENCE OF CRACKS,BURRS, LOOSE CONTACTS, 
CONTACT ALIGNMENT, VOIDS,FLAWS OR ANY FOREIGN MATTER DETRIMENTAL TO THE FUNCTION OF 

THE CONNECTOR. CONTACT MATING SURFACES SHALL BE FREE FROM CRACKS, BURRS, BENDS AND 

FOREIGN PARTICLES. x 

3. . DESIGN REQUIREMENTS: 

A. MAXIMUM WORKING VOLTAGE: 250 VOLTS DC, 175 VOLTS RMS. 

B. DIELECTRIC WITHSTANDING VOLTAGE: 100.000 FEET: 250 VOLTS RMS. PER METHOD 301 OF MIL-STD-202 

C. CURRENT RATING: 3 AMPERES RMS MAXIMUM 

D. CONTACT VOLTAGE DROP: 25 MILLIVOLIS, MAXIMUM AT 3 AMPERES DC. 

E. INSERTION AND WITHDRAWAL: (WITH MATING CONNECTOR) INDIVIDUAL CONTACTS SHALL 
HAVE A MAXIMUM ENGAGEMENT FORCE OF 6 OUNCES AND A MINIMUM WITHDRAWAL FORCE OF 
.5 OUNCES. ASSEMBLIES SHALL NOT EXCEED A MATING FORCE EQUAL TO THE PRODUCT OF 

THE NUMBER OF CONTACTS X 7.5 OUNCES OR BE LESS THAN A MINIMUM WITHDRAWAL FORCE EQUAL TO THE PRODUCT 
OF THE NUMBER OF CONTACTS X 1 OUNCE.I NIT I ALLY - 0.5 OUNCES AFTER LIFE. 

F. CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT OF THE CONNECTOR AT 120 CYCLES/HOUR MAX, 

THE CONTACT VOLTAGE DROP SHALL BE 35 MV AT 3 ADC AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 

G. DIELECTRIC MATERIAL: (BODY) DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-19833, GDI-30. 

H. LEADS: SHALL BE 28 STRANDED WIRE, TEFLON INSULATED, PER MIL-W-16878. TYPE ET, 

COLOR CODED PER TABLE I. 

(1) LEADS SHALL WITHSTAND A 4 LB AXIAL PULL (APPLIED GRADUALLY)FOR 10 SECONDS. 

I. CAPTIVE SCREW: CRES TYPE 303 PER MIL-S-7720, PASSIVATED PER FINISH 5.4.2 OF MIL-STD-171 

J. MOUNTING PLATE: BRASS, TIN PLATED PER MIL-T-10727, TYPE I, FUSED OVER COPPER FLASH. 

K. STUD: STEEL. TIN PLATED PER MIL-T-10727, TYPE I, FUSED OVER COPPER FLASH. INTERNAL THREADS TO 
BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENED SECURELY AND HERMETICALLY SEALED 

TO MOUNTING PLATE. ___ 

UNLESS OTHERWISE SPECIFIED 

-;— DIMENSIONS ARE IN INCHES 

_TOLERANCES ON 

FRACTIONS DECIMALS / 


REVISIONS 

_ DESCRIPTION _ 

REPLACES SHEET 1 REV B 
WITH CHANGES |OPf 
REVISED PER TDRR II142 
REVISED PER TDRR 11998 
'REVISED PER tDRR l4?9< 


DATE APPROVAL 




©REPLACES SHEET I REV B WITH CHANGES 


PART OR 
IDENTIFYING NO. 


INSTRUMENTATION LAB 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND 1002034 FOR THIS DRAWING 


FRACTIONS 
± -**■ 


ANGLES DRAWN « 


DATE 7-/-^ 

4 + 


APPLICATION 


DO NOT SCALE THIS DRAWING 
MATERIAL 

AS SHOWN 

HEAT TREATMENT 


FINAL FINISH 

AS SHOWN 


NASA APPROVAL 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 

CONNECTOR, ELECTRICAL 

25 CONTACTS,PLUG £ RECEPTACLE 

,_ SPECIFICATION CONTROL DRAWING 

CODE IDENT NO. I SIZE I NASA DRAWING NO. 

















Il 


n 

m 


a: 


i 


f 


NOTICE — WHEN GOVERNMENT DRAWINGS. SPECIFICATIONS. OR OTHER DATA 
ARE USEO FOR ANY PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
RELATED GOVERNMENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN¬ 
MENT THEREBY INCURS NO RESPONSIBILITY NOR ANY OBLIGATION WHATSOEVER; 
AND THE FACT THAT THE GOVERNMENT MAY HAVE FORMULATED. FURNISHED. OR 
IN ANY WAY SUPPLIED THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO BE REGARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSING THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY¬ 
ING ANY RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL ANY 
PATENTED INVENTION THAT MAT IN ANY WAY BE RELATED THERETO. 


Z617I00I 


L. VIBRATION; DURING VIBRATION PER ND 1002052, DISCONTINUNITY SHALL BE 0-1 MICROSECOND 
OR LESS. AT 100 MA DC FOR MATED CONNECTORS. 

M. CONTACT RESISTANCE: 10 Ml LLI0HMS MAX AT 100 MADC TEST PER MIL-STD-202, METHOD 307. (MATED _ PA IRS ) 

N. TEMPERATURE OPERATING: -55°C TO +150°C. 


| REVISIONS 10*14 ll 

SYM 

DESCRIPTION 

DATE 

APPROVAL 

c 

THIS SHEET ADDED (o9 7f 

WT 

m 

D 

REVISED PER TDRR 11142 


ML 

\ E 

REVISED PER TDRR 11998 

w* 

< 

rr 

REVISED PER TDRR 14790 


J4L 


4. 


A. 


SPECIAL REQUIREMENTS: (BY SUPPLIER) 

CONTACT SEPARATION: (100% INSPECTION) ALL PIN CONTACTS SHALL BE TESTED WITH A 


B. 


STEEL TEST SLEEVE HAVING AN INSIDE DIAMETER OF .0230 +00dl AND FINISH OF 16 

-0000 

MICRO-INCHES MAX. THE TOTAL WEIGHT OF THE TEST SLEEVE SHALL BE .5 OUNCES +.1 

-.0 

WHEN THE ASSEMBLY IS INVERTED THE PIN CONTACT SHALL RETAIN THE .5 OUNCE WEIGHT. 

THIS TEST SHALL BE PERFORMED SEQUENTIALLY ON EACH CONTACT AFTER ASSEMBLY WITH THE CONNECTOR BODY. 

THE FOLLOWING LOT SAMPLE TESTS SHALL BE MADE PPIOR TO 

shipment: 

(1) TENSILE STRENGTH: 

THE CRIMPED ASSEMBLIES FROM EACH TOOL SHALL BE SAMPLED PER MIL-STD-414 

INSPECTION LEVEL IV, AQL .4. THE ASSEMBLIES SHALL BE TESTED ON A HUNTER SCALE (OR EQUIVALENT) 

FOR TENSILE STRENGTH AND THE READINGS SHALL BE RECORDED. ALL ASSEMBLIES 
SHALL BE WITHIN THE CONTROL LIMITS STATED BELOW OR THE LOT SHALL BE 

REJECTED. ASSEMBLIES SHALL BE PACKAGED AND IDENTIFIED WITH THE LOT NUMBER, 

WHICH SHALL ACCOMPANY THE UNITS TO FINAL INSPECTION, AND BE INCLUDED WITH 
THE CONNECTOR SHIPMENT. THIS APPLIES TO BOTH PINS AND SOCKETS. 

THERE SHALL BE TWO DATA SHEETS FOR THE CRIMP I, T OF THE PINS, ONE FOR THE PIN END 
AND ONE FOR THE WIRE END. 



PIN 

SOCKET 

WIRE 

CONTACT 

WIRE 

WIRE 

SIZE 

END (MIN) 

END (MIN) 

END (MIN) 

28 

3.0 LBS 

4.0 LBS 

4.0 LBS 


(2) 


SOCKET STRENGTH, SIDE LOAD (IN CONNECTOR): 18 OUNCES MINIMUM SHALL BE APPLIED AT 

THE PIN ENGAGING END OF THE SOCKET. INTERMATABILITY AND PERFORMANCE SHALL NOT BE 
IMPAIRED. 


MATING AND CLEANING: (100% INSPECTION) EACH CONNECTOR SHALL BE MATED 5 TIMES AND THEN 
ULTRASONICALLY CLEANED FOR 1/2 MINUTE. INSPECT FOR LOOSE, CRUSHED OR MISALIGNMENT 
OF CONTACTS. 


© THIS SHEET ADDED 


QTY 

PART OR 

NOMENCLATURE OR 

FIND 

REQD 

IDENTIFYING NO. 

DESCRIPTION 

NO. 
















NEXT ASSY 

USED ON 

| APPLICATION | 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MATERIAL 

AS SHOWN 


HEAT TREATMENT 


FINAL FINISH 

AS SHOWN 


E 


LIST OF MATERIALS 


M I T 

INSTRUMENTATION LAB 
Cambmiooc. Mass. 

G. WO._COMTMCT_ 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


DRAWN rf DATE 7- 

CHECKED 
APPROVAI (Ji 


APPROVAL 



CONNECTOR, ELECTRICAL 

25 CONTACTS,PLUG £ RECEPTACLE 


SPECIFICATION CONTROL DRAWING 


NASA APPROVAL 


CODE IDENT NO. 


MIT APPROVAL 


SCALE 


SIZE 


NASA DRAWING NO. 

1001497 


WT 


| SHEET Z OF 3 


$ - f 


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REVISIONS TQft 


/ so/? a’2*/ 0/000 

SHEET I REDRAWN REPLACED BY 
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PER TDRR __ 

' REVISED PER TDRR lot 7 : 

REVISED PER TDRR I I 142 < 

’ REVISED PER TDRR 11998 i 

REVISED PER TDRR 14790 ' 


\(A w/d 

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M I T 

INSTRUMENTATION LAS 
Camvmdm, mam. 


UNLESS OTHERWISE SPECIFIED M 1 

DIMENSIONS ARE IN INCHES * NST, cVSimEi 

TOLERANCES ON wi wo. _ 

FRACTIONS DECIMALS ANGLES DRAWN T//6W0 

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DATE^/^ 1 


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I FINAL FINISH 


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AS SHOWN 


APPROVAL 
NASA APPROVAL ] 


MU APPROVAL ! 


NOMENCLATURE OR FIN 

DESCRIPTION NO 

LIST OF MATERIALS 

MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 

coA/A/rcro/?, nrcTye/c/u 

2S C0/V7XCTS, /*ll/C g jes-Cf/*™ Cl & 
jr/7Fe//=ycAr/OAf co//r*#i /?A4yv/A/c 


I CODE IDENT NO. SIZE 




NASA DRAWING NO. 

1001497 


SHEET 3 OF 3 


4 























ugaa 


3 


2 


NOTICE - WHIM GOVERNMENT 0* A WINS*. SPECIFICATIONS. OR OTHER DATA 
ARC USED FOR ANT PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
RELATED GOVERNMENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN¬ 
MENT THEREST INCURS NO RESPONSIGILITT NOR ANT OBLIGATION WHATSOEVER: 
AND THE FACT THAT THE GOVERNMENT MAT HAVE FORMULATED. FURNISHED. OM 
IN ANT WAT SUPPLIED THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO DC REGARDED GT IMPLICATION OR OTHERWISE AS IN ANT MANNER 
LICENSING THE HOLDER OR ANT OTHER PERSON °* CORPORATION.ORCONVET- 
IN6 ANT RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL AMT 
PATENTED INVENTION THAT MAT IN AMT WAT RE RELATEO THERETO. 


REQUIREMENTS: 

GENERAL 

A INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

UNITS SHALL BE CAPABLE OF MEETING THE APPLICABLE REQUIREMENTS OF MIL-C-8384. EXCEPT AS 

c! SSpIMTcSfJS »?»?“?!!« SPEC,mo .. » 10*04. CLOSS 1. 

0. UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPEC!FIED *J [J^J. 002052 
UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS SECTION (3) OF THIS DRAWING. 

E. PACKAGING AND PACKING:UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
* MARKED WITH THE DRAWING NUMBER (1001491). REVISION LETTER, DASH NUMBER f 

THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING DATE 
/ OR CODE. UNITS SHALL BE INDIVIDUALLY PACKAGED PER ND I0022l5r, CLASS I 

F. MARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001491), REVISION 

LETTER AND DASH NUMBER SHALL BE MARKED ON THE UNIT PER ND 1002019. 


REVISIONS 

DEfCWIPTION 

' REPLACES SHEET I REV B 
WITH CHANGES |OPf 
' REVISED PER TDRR 11142 
REVISED PER TDRR 11998 
' REVISED PER TDRR 14796 
'REVISED PER TDRR 17500 


PATE APPROVAL 

mL<4 .... 



ACCEPTANCE AND INSPECTION 
DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 900 VOLTS RMS MINIMUM PER METHOD 301 OF M'JL-STD-202 

INSULATION RESISTANCE: 200K MEGOHMS, MINIMUM AT 500 VOLTS DC PER METHOD 302 OF MIL-STD-202. 

DIMENSIONS AS SPECIFIED HEREIN. rnwTArT<; 

100* INSPECTION: INSPECT OPTICALLY 10 X MAGNIFICATION FOR EVIDENCE OF CRACKS,BURRS, LOOSE CONTACTS, 
CONTACT ALIGNMENT, VOIDS.FLAWS OR ANY FOREIGN MATTER DETRIMENTAL TO THE FUNCTION OF 
THE CONNECTOR. CONTACT MATING SURFACES SHALL BE FREE FROM CRACKS, BURRS, BENDS AND 
FOREIGN PARTICLES. 


DESIGN REQUIREMENTS: 

MAXIMUM WORKING VOLTAGE: 250 VOLTS DC, 175 VOLTS RMS. 

DIELECTRIC WITHSTANDING VOLTAGE: 100,000 FEET: 250 VOLTS RMS. PER METHOD 301 OF MIL-STD-202 
CURRENT RATING: 3 AMPERES RMS MAXIMUM 

CONTACT VOLTAGE DROP: 25 MILLIVOLIS, MAXIMUM AT 3 AMPERES DC. 

INSERTION AND WITHDRAWAL: (WITH MATING CONNECTOR) INDIVIDUAL CONTACTS SHALL 
HAVE A MAXIMUM ENGAGEMENT FORCE OF 6 OUNCES AND A MINIMUM WITHDRAWAL FORCE OF 
.5 OUNCES. ASSEMBLIES SHALL NOT EXCEED A MATING FORCE EQUAL TO THE PRODUCT OF 

THE NUMBER OF CONTACTS X 7.5 OUNCES OR BE LESS TMAM A MINIMUM WITHDRAWAL FORCE EQUAL TO THE PRODUCT 

OF THE NUMBER OF CONTACTS X 1 OUNCE.INITIALLY - 0.5 OUNCES AFTER LIFE. ' „ /Llrtll _ „ AV 

CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT OF THE CONNECTOR AT 120 

THE CONTACT VOLTAGE DROP SHALL BE 35 MV AT 3 ADC AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 
DIELECTRIC MATERIAL: (BODY) DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-I4,TYPE SDG 
LEADS: SHALL BE 28 STRANDED WIRE, TEFLON INSULATED, PER-MIL-W-16878. TYPE ET. 

COLOR COOED PER TABLE I. 

(1) LEADS SHALL WITHSTAND A 4 LB AXIAL POLL(APPLIED GRADUALLY)FOR 10 SECONDS. 

CAPTIVE SCREW: CRES TYPE 303 PER MIL-S-7720, PASSIVATED PER FINISH 5.4.2 OF MIL-STD-171 

MOUNTING PLATE: BRASS. TIN PLATED PER MIL-T-10727. TYPE I , FUSED OVER COPPER FLASH. 

STUD: STEEL. TIN PLATED PER MIL-T-10727. TYPE I , FUSED OVER COPPER FLASH. INTERNAL THREADS TO 
BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENED SECURELY AND HERMETICALLY SEALED 

TO MOUNTING PLATE. i | I unless otherwise SP 


©REPLACES SHEET I REV B WITH CHANGES 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES IN 

TOLERANCES ON — * 

FRATIONS DECIMALS ANGLES DRAW N 


PART OR 
IDENTIFYING NO. 


INSTRUMENTATION LAB 
Cambridok. MASS. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND 1002034 FOR THIS DRAWING 


APPLICATION 


DO NOT SCALE THIS DRAWING 
MATERIAL 

AS SHOWN 

HEAT TREATMENT 

FINAL FINISH 

AS SHOWN 


CHECKED 

APPROVA^ 

APPROVAL. 


I NASA APPROVAL 


MIT APPROVAL J 


DATE l-y-^ 

4 -j-i-ti 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 

CONNECTOR, ELECTRICAL 

25 CONTACTS, PLUG < RECEPTACLE 

SPECIFICATION CONTROL DRAWING 

CODE IDENT NO. I SIZE I NASA DRAWING NO. 

Q 1001497 

SCALE WT I SHEET j Of 3 


3 













NOTICE — WHEN GOVERNMENT DRAWINGS. SPECIFICATIONS. ON OTMEN DATA 
ANE USED PON ANT PUNPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
DELATED GOVENNMENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN* 
NENT THEREST INCURS NO RESPONSIBILITY NON ANT OBLIGATION WHATSOEVER; 
ANO THE FACT THAT THE GOVERNMENT MAT HAVE FORMULATED. FURNISHED. OR 
IN ANT WAY SUPPLIED THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO BE NE6AR0ED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSING THE HOLDER OR ANT OTHER PERSON OR CORPORATION. OR CONVEY* 
INC ANY RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR BILL AMY 
PATENYEO INVENTION THAT HAT IN ANY WAY BE RELATED THERETO. 


L. VIBRATION: OUR I NO VIBRATION PER NO 1002052. DISCONTINUNITY SHALL BE Q.1 MICROSECOND 

OR LESS. AT 100 MA DC FOR MATEO CONNECTORS. , mT „ DAlD ,,T 

M. CONTACT RESISTANCE: 10 MILL I OHMS MAX AT 100 MADC TEST PER MIL-STD-202, METHOD 307. I M AT ED PA IRS 1 

N. TEMPERATURE OPERATING: -55°C TO ♦150 , C. 


. . SPECIAL REQUIREMENTS: (BY SUPPLIER) 

A. CONTACT SEPARATION: (100* INSPECTION) ALL PIN CONTACTS SHALL BE TESTED WITH A 
STEEL TEST SLEEVE HAVING AN INSIDE DIAMETER OF .0230 +000^ flND FINISH OF 16 
MICRO-INCHES MAX. THE TOTAL WEIGHT OF THE TEST SLEEVE SHALL BE .5 OUNCES O 

WHEN THE ASSEMBLY IS INVERTED THE PIN CONTACT SHALL RETAIN THE .5 OUNCE WEIGHT. 

THIS TEST SHALL BE PERFORMED SEQUENTIALLY ON EACH CONTACT AFTER ASSEMBLY WITH THE CONNECTOR BODY. 

B. THE FOLLOWING LOT SAMPLE TESTS SHALL_BE MADE PPIOR TO 

SHIPMENT! . 

- 1 * THE^CIHMPED^ASSEMBLIES FROM EACH TOOL SHALL BE SAMPLED PER MIL-STD-414 

INSPECTION LEVEL IV. AQL .4. THE ASSEMBLIES SHALL BE TESTED ON A HUNTER SCALE (OR EQUIVALENT) 

FOR TENSILE STRENGTH AND THE READINGS SHALL BE RECORDED. ALL ASSEMBLIES 
SHALL BE WITHIN THE CONTROL LIMITS STATED BELOW OR THE LOT SHALL BE 

REJECTED. ASSEMBLIES SHALL BE PACKAGED AND IDENTIFIED WITH THE LOT NUMBER. 

WHICH SHALL ACCOMPANY THE UNITS TO FINAL INSPECTION. ANO BE INCLUDED WITH 
THE CONNECTOR SHIPMENT. THIS APPLIES TO BOTH PINS AND SOCKETS. 

THERE SHALL BE TWO DATA SHEETS FOR THE CRIMPING OF THE PINS, ONE FOR THE PIN END 
AND ONE FOR THE WIRE END. 


Z.617IOOI 


REVISIONS 

j Y M | DESCRIPTION 

~ THIS SHEET ADDED /0#7<f 
IT REVISED PER TDRR 11142 
E REVISED PER TDRR 11998 
~F~ REVISED PE R TDRR I4790~ 
IT REVISED PER TDRR 17500 


'toL'l 

Bi 


CONTACT 

END 

3.0 LBS 


4.0 LBS 


SOCKET 


4.0 LBS 


(?) SOCKET STRENGTH, SIDE LOAD (IN CONNECTOR): 18 OUNCES MINIMUM SHALL BE APPLIED AT 
' THE PIN ENGAGING END OF THE SOCKET. INTERMATABILITY AND PERFORMANCE SHALL NOT BE 

t IMPAIRED. 

C MATING AND CLEANING: (100% INSPECTION) EACH CONNECTOR SHALL BE MATED 5 TIMES AND THEN 
ULTRASONICALLY CLEANED FOR 1/2 MINUTE. INSPECT FOR LOOSE, CRUSHED OR MISALIGNMENT 
OF CONTACTS. 


© THIS SHEET ADDED 



APPLICATION 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES >N 

TOLERANCES ON —• "9 

FRACTIONS DECIMALS ANGLES DRAWN 
± ± ± 

CHECKE 

DO NOT SCALE THIS DRAWING APPROV 


PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAB 
Cammiogb, Mam. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


AS SHOWN 

HEAT TREATMENT 


I FINAL FINISH 


AS SHOWN 


I NASA APPROVAL. 


MIT APPROVAL 1 


CONNECTOR, ELECTRICAL 

~~ 25 CONTACTS.PLUG $ RECEPTACLE 

7 _ SPECIFICATION CONTROL DRAWING 

J CODE IDENT NO.I SIZE NASA DRAWING NO. 

uilli cl 1001497 

p-lfSl Q SCALE WT I SHEET 2 OF 3 






















16 171001 


REVISIONS TDA 


XT’S X//XST / XO/r XSMOAtX 


SHEET I REDRAWN REPLACED BY 
REV C WITH CHANGES 
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i 


iwimn. mcmcATiom. oa oymnn data 

AM HMD PON ART PUNPOM OTNII THAN IN CONHKCTIO** WITH A OtPmtTtLT 
MUTII AOVCAHHirr PMCUMNINT OtYNATKMI. TNC UNITES (TATIS NOVSiN- 
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AM TNI PACT THAT TNI MVtANNINT NAT NAVI PMNWlATtO. PVNNIINIO. ON 

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IM ANT NIAMTA ON PINNI A AION TO NANUPACTWM. NM. WN ASLL ANT 
NATINTSN I NM NT ION THAT NAT IN ANT WAT Al M LATIN TNINITO. 


86171001 


REQUIREMENTS: 

1. GENERAL: 

A. INTERPRET ORAUING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY HIL-D-70327. 
UNITS SHALL BE CAPABLE OF NEETING THE REQUIREHENTS OF HIL-C-8384, EXCEPT AS 


B. 


D. 


E. 


F. 


| REVISIONS | 

EZI 


DATS 


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uses 






AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN 
NO 1015404, CLASS 2. 

UNITS SHALL BE CAPABLE OF NEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED 
IN NO 1002052 UNLESS MODIFIED OR AMMENDEO BY THE DESIGN REQUIREMENTS 
SECTION (3) OF THIS ORAWING. 

PACKAGING ANO PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE ORAWING NUMBER (1001498), REVISION LETTER, DASH NUMBER (IF ANY), 

THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING 
OATE OR CODE. 

NARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001498), REVISION LETTER, 
AND DASH NUMBER (IF ANY) SHALL BE MARKEO ON THE PART PER MIL-STD-130. 


2 . 


3. 


ACCEPTANCE AND INSPECTION 

A. DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 750 VOLTS, HNS Mlfc 

B. INSULATION RESISTANCE: ZOOK MEGOHMS, MINIMUM AT 500 VOLTS DC. 

DESIGN REQUIREMENTS: 

A. MAXIMUM WORKING VOLTAGE: 250 VOLTS DC. 

01ELECTRIC WITHSTANDING VOLTAGE; 100,000 FEET: 500 VOLTS RMS. 

CURRENT RATING: 3 AMPERES RMS, MINIMUM. 

CONTACT VOLTAGE DROP: 25 MILLIVOLTS, MAXIMUM AT 3 AMPERES DC. 

INSERTION ANO WITHDRAWAL FORCE (WITH MATING CONNECTOR): 2 OUNCES MINIHUM- 
4 OUNCES MAXIMUM, PER CONTACT. 

CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT ANO DISENGAGEMENT THE CONTACT 


B. 

C. 
0. 
E. 


F. 

VOLTAGE DROP AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 

G. 01ELECTRIC MATERIAL: DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-14, TYPE SDG. 

H. LEAOS: SHALL BE 128 STRANDED LEADS, TEFLON INSULATED. PER MIL-W-16878, 

TYPE ET,.COLOR CODED PER TABLE I. 

X. CAPTIVE SCREW: I2-5BNC-2A CAPTIVE SCREW; STEEL. WITH A CADMIUM PLATE. 

J. MOUNTING PLATE: BRASS, WITH FUSED ELECTRO-TIN ON CADMIUM PLATE OVER COPPER FLASH. 

K. STUD: I2-56NC-2B TAPPED STUD; STEEL, WITH FUSED ELECTRO-TIN ON CADMIUM PLATE OVER COPPER FLASH. 
INTERNAL THREADS TO BE FREE OF ELECTRO-TIN PLATING. STUO SHALL BE FASTENED SECURELY AND 
HERMETICALLY SEALED TO MOUNTING PLATE. 

L. VIBRATION: DURING VIBRATION PER NO 1015404, DISCONTINUITY SHALL BE 1 NICROSECONO OR LESS. 


QTV 

PART OR 

NOMENCLATURE OR 

FINO 

REQD 

IDENTIFYING NO. 

DESCRIPTION 

NO. 


PROCURE ONLY FROM APPROVEO SOURCES LISTED.IN 
NO 1002034 FOR THIS ORAWING. 
















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DRAWN TT/e/SQ DATE ^/^ i 
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CODE IDENT NO. 


SCALE 


SIZE 


NASA DRAWING NO. 

1001498 


WT 


[SHEET / OF £ 


I 2 

PHOTOGRAPHIC SCALE ONLY 


































REQUIREMENTS: 

1. GENERAL: 


A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. UNITS SHALL BE CAPABLE OF MEETING THE REQUIREMENTS OF MIL-C-8384, EXCEPT AS 
AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

C. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN 
ND 1015404, CLASS 2. 

D. UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED 
IN ND 1002052 UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS 
SECTION (3) OF THIS DRAWING. 

E. PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001498), REVISION LETTER, DASH NUMBER (IF ANY), 

THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING 
DATE OR CODE. 

F. MARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001498), REVISION LETTER, 
AND DASH NUMBER (IF ANY) SHALL BE MARKED ON THE PART PER MIL-STD-130. 

2. ACCEPTANCE AND INSPECTION 

A. DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 750 VOLTS, RMS Hllf* 

B. INSULATION RESISTANCE: BOOH MEGOHMS, MINIMUM AT 500 VOLTS DC. 

3. DESIGN REQUIREMENTS: 

A. MAXIMUM WORKTNG VOLTAGE: 250 VOLTS DC. 

B. DIELECTRIC WITHSTANDING VOLTAGE; 100,000 FEET: 500 VOLTS RMS. 

C. CURRENT RATING: 3 AMPERES RMS, MINIMUM. 

D. CONTACT VOLTAGE DROP: 25 MILLIVOLTS, MAXIMUM AT 3 AMPERES DC. 

E. INSERTION AND WITHDRAWAL FORCE (WITH MATING CONNECTOR): 2 OUNCES MININUM- 
4 OUNCES MAXIMUM, PER CONTACT. 

F. CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT THE CONTACT 

VOLTAGE DROP AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 

G. DIELECTRIC MATERIAL: DIALLYL PHTHALATE, GLASS FILLED PER MlL-M-14, TYPE SDG. 

H. LEADS: SHALL BE 128 STRANDED LEADS, TEFLON INSULATED, PER MIL-W-16878, 

TYPE ET,.COLOR CODED PER TABLE X. 

X. CAPTIVE SCREW: I2-5GNC-2A CAPTIVE SCREW; STEEL, WITH A CADMIUM PLATE. 

J. MOUNT IN6 PLATE: BRASS, WITH FUSED ELECTRO-TIN ON CADMIUM PLATE OVER COPPER FLASH. 

K. STUD: I2-5GNC-2B TAPPED STUD; STEEL, WITH FUSED ELECTRO-TIN ON CADMIUM PLATE OVER COPPER 

INTERNAL THREADS TO BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENED SECURELY AND 

HERMETICALLY SEALED TO MOUNTING PLATE. 

L. VIBRATION: DURING VIBRATION PER ND 1015404, DISCONTINUITY SHALL BE 1 MICROSECOND OR LESS. 


PROCURE ONLY FROM APPROVED SOURCES LISTED .IN 
ND 1002034 FOR THIS DRAWING. 



APPLICATION 


2 





86171001 


REVISIONS 
DcscnipnoN ' 

r/rtier /, s»tirr~, 

to CLASS A 

-rtlf.Oi/fir 

AA«e» A****** *7*rus 
REPLACED BY REV C 
PER TDRR IO?7S" 


DATA I APfllOVAL 




m 




l 


REPLACED BY REV C WITH CHANGES 


tey/s/c?// *7/4rc/s sweerf 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES ,Nr 

TOLERANCES ON — », 

FRACTIONS DECIMALS ANGLES qrawN > 

£ _ ± _ ± _ U 

CHECKED 

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MATERIAL “ 

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PART OR 
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INSTRUMENTATION LAB 


. DATE^^fl 


I HEAT TREATMENT 


I FINAL FINISH 


NASA APPROVAL, 


NOMENCLATURE OR F 

DESCRIPTION f 

LIST OF MATERIALS 

MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 

C0/v/yr(rr6>/e, /rurcr/r/csi 

CA r/£>/v cowreoi &AAWW* 

"fcoOE IDENT NO. | SIZE I NASA DRAWING NO. 




I MIT APPROVj 




NASA DRAWING NO. 

1001498 






































3 


2 


NOTICE — WHEN •OVERNMCNT DRAWINGS. SPECIFICATIONS. OR OTHER DATA 
ARE USED FOR ART PURPOSE OTHER THAR IR COHHCCTIOR WITH A DEFIRITELY 
RELATED GOVERNMENT PROCUNEMENT OPERATIOR. THE URITED STATES GOVERN- 
■ENT THERERT INCURS NO RESPONSIBILITY NOR ANY ONLICATION WHATSOEVER; 
ANO THE FACT THAT THE GOVERNMENT MAY HAVE FORMULATED. FURNISHED. OR 
IN ART WAY SUPPLIEO THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO BE REGARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSING THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY¬ 
ING ANY RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL ANT 
PATENTED INVENTION THAT NAT IN ANY WAY RE RELATED THERETO. 



REVISIONS 


D[K»IPTKW 


REPLACES SHEET I REV B 
WITH CHANGES tOflf 


mrnul 


A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. UNITS SHALL BE CAPABLE OF MEETING THE REQUIREMENTS OF MIL-C-8384. EXCEPT AS 
AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

C. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND 1015404, CLASS 2. 

D. UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED IN ND 1002052 
UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS SECTION (3) OF THIS DRAWING. 

E. PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001498). REVISION LETTER, DASH NUMBER 

THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER ANO THE MANUFACTURING DATE 
OR CODE. UNITS SHALL BE INDIVIDUALLY PACKAGED PER ND 1002215, CLASS I 

F. MARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001498), REVISION 

LETTER AND DASH NUMBER SHALL BE MARKED ON THE UNIT PER ND 1002019. 


ACCEPTANCE AND INSPECTION 
DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL:, 900 VOLTS RMS MINIMUM PER METHOD 301 OF MIL-STD-202 

INSULATION RESISTANCE: 200K MEGOHMS, MINIMUM AT 500 VOLTS DC PER METHOD 302 OF MIL-STD-202. 
DIMENSIONS AS SPECIFIED HEREIN. 

100* INSPECTION: INSPECT OPTICALLY FOR EVIDENCE OF CRACKS, BURRS, LOOSE CONTACTS, 

CONTACT ALIGNMENT, VOIDS, FLAWS OR ANY FOREIGN MATTER DETRIMENTAL TO THE FUNCTION OF 
THE CONNECTOR. CONTACT MATING SURFACES SHALL BE FREE FROM CRACKS, BURRS, BENDS AND 
FOREIGN PARTICLES. 


DESIGN REQUIREMENTS: 

MAXIMUM WORKING VOLTAGE: 250 VOLTS DC, 17S VOLTS RMS. 

DIELECTRIC WITHSTANDING VOLTAGE: 100,000 FEET: 250 VOLTS RMS. PER METHOD 301 OF MIL-STD-202 
CURRENT RATING: 3 AMPERES RMS,MINIMUM. 

CONTACT VOLTAGE DROP: 25 MILLIVOLTS, MAXIMUM AT 3 AMPERES DC. 

INSERTION AND WITHDRAWAL: (WITH MATING CONNECTOR) INDIVIDUAL CONTACTS SHALL 
HAVE A MAXIMUM ENGAGEMENT FORCE OF 6 OUNCES AND A MINIMUM WITHDRAWAL FORCE OF 
.5 OUNCES. ASSEMBLIES SHALL NOT EXCEED A MATING FORCE EQUAL TO THE PRODUCT OF 
THE NUMBER OF CONTACTS X 7.5 OUNCES OR A WITHDRAWAL FORCE EQUAL TO THE PRODUCT 
OF THE NUMBER OF CONTACTS X 1 OUNCE. 


CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT OF THE CONNECTORS "AT 120 CYCLES/HOUR MAX, /«\ nppi A^CC CUCpT \ new o WITH PHANC5FQ 

THE CONTACT VOLTAGE DROP AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. r\C.r I i rvuv D VVI I n wnHi’ivjc.O 


DIELECTRIC MATERIAL: (BODY) DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-19833, GDI-30. 
LEADS: SHALL BE 28 STRANDED WIRE, TEFLON INSULATED, PER MIL-W-16878. TYPE ET, 

COLOR CODED PER TABLE I. j 

(1) LEADS SHALL WITHSTAND A 4 LB AXIAL PULL (APPLIED GRADUALLY)FOR 10 SECONDS. 

CAPTIVE SCREW: CRES TYPE 303 PER MIL-S-7720, PASSIVATED PER FINISH 5.4.2 OF MIL-STD-171 
MOUNTING PLATE: BRASS, TIN PLATED PER MIL-T 7 10727, TYPE I OVER COPPER FLASH. 

STUD: STEEL. TIN PLATED PER MIL-T-10727, OVER COPPER FLASH. INTERNAL THREADS TO 

BE FREE OF ELECTRO-TIN P.LATING. STUD SHALL BE FASTENED SECURELY AND HERMETICALLY SEALED 
TO MOUNTING PLATE. 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND 1002034 FOR THIS DRAWING 


UNLESS OTHERWISE SPECIFIED M 1 T 

DIMENSIONS ARE IN INCHES * NST LA “ 

TOLERANCES ON png no. 

FRACTIONS DECIMALS ANGLES drawn "Tump 

* * CHECKED P7\0 


DO NOT SCALE THIS DRAWING 
MATERIAL 

AS SHOWN 

HEAT TREATMENT 


NEXT 'ASSY 


FINAL FINISH 


APPLICATION 


as Shown 


APPROVAL. 


NASA APPROVAL/ 


MIT APPROVAL 


MANNED SPACECRAFT CENTER 
HOUSTON, TEXAS 

CONNECTOR ELECTRICAL 

37 CONTACTS PLUG $ RECEPTACLE 

SPECIFICATION CONTROL DRAWING 


CODE IDENT NO. SIZE 



NASA DRAWING NO. 

1001498 


I SHEET | OF 3 


wnsw 




















REVISIONS 


NOTICE — WHEN GOVERNMENT DRAWINGS. SPECIFICATIONS. OR OTHER DATA 
ARE USED FOR ANY PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
RELATED GOVERNMENT PROCUREMENT OPERATION. THE UNITEO STATES GOVERN¬ 
MENT THCRCRY INCURS NO RFSPONSIRILITY NOR ANY ORLI6ATION WHATSOEVER: 
AMO THE FACT THAT THE GOVERNMENT MAY HAVE FORMULATEO. FURNISHED. OR 
IN ANY WAY SUPPLIED THE SAIO DRAWINGS. SPECIFICATIONS ON OTHER DATA IS 
ROT TO RE REGARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSING THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY- 
INC ANY RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL AMY 
PATENTED INVENTION THAT MAY IN ANY WAY RE RELATED THERETO. 


to% ?r 


DESCRIPTION 


THIS SHEET ADDED 

TDRR idgys" _ 


L. VIBRATION: DURING VIBRATION PER NO 1002052, DISCONTINUITY SHALL BE 0.1 MICROSECOND 
OR LESS, AT 100 MA DC FOR MATED CONNECTORS. 

M. CONTACT RESISTANCE: 10 MILLI OHMS MM: AT 100 MADC TEST PER MIL-STD-202, METHOD 307. (HATED PAIRS) 

N. TEMPERATURE OPERATING: -55 # C TO ♦150 , C. 


SPECIAL REQUIREMENTS: (BY SUPPLIER) 

CONTACT SEPARATION: (100%*INSPECTION) ALL PIN CONTACTS SHALLBE TESTED WITH A 
STEEL TEST SLEEVE HAVING AN INSIDE DIAMETER OF .0230 AND FINISH OF 16 

MICRO-INCHES MAX. THE TOTAL WEIGHT OF THE !£Sf SLEEVE SHALL BE .5 OUNCES +.J 

WHEN THE ttKMBLY IS INVERTED THE PIN CONTACT SHALL RETAIN THE .5 OUNCE WEIGHT. 

THIS TEST SHALL BE PERFORMED ON THE CONTACTS PRIOR TO ASSEMBLY WITH ItttONNECTOR BODY. 

THE FOLLOWING LOT SAMPLE TESTS SHALL BE MADE PRIOR TO- 

shipment: 

(1) TENSILE STRENGTH: 

THE CRIMPED ASSEMBLIES FROM EACH TOOL SHALL BE SAMPLED PER MIL-STD-414 
INSPECTION LEVEL IV, AQL .4. THE ASSEMBLIES SHALL BE TESTED ON A HUNTER SCALE 
FOR TENSILE STRENGTH AND THE READINGS SHALL BE RECORDED. ALL ASSEMBLIES 
r SHALL BE WITHIN THE CONTROL LIMITS STATED BELOW OR THE LOT SHALL BE 
REJECTED. ASSEMBLIES SHALL BE PACKAGED AND. IDENTIFIED WITH THE LOT NUMBER, 

WHICH SHALL ACCOMPANY THE UNITS TO FINAL INSPECTION, AND BE INCLUDED WITH 
THE CONNECTOR SHIPMENT. THIS APPLIES TO BOTH PINS AND SOCKETS. 

THERE SHALL BE TWO DATA SHEETS FOR THE CRIMPING OF THE PINS, ONE FOR THE PIN END 
AND ONE FOR THE WIRE END, 


CONTACT 
END (Ml 
3.0 LBS 


4.0 LBS 


SOCKET 


4.0 LBS 


(2) SOCKET STRENGTH, SIDE LOAD (IN CONNECTOR): 18 OUNCES MINIMUM SHALL BE APPLIED AT 
THE PIN ENGAGING END OF THE SOCKET. INTERMATABILITY AND PERFORMANCE SHALL NOT BE 
IMPAIRED. 

2. MATING AND CLEANING: (lOO% INSPECTION) EACH CONNECTOR SHALL BE MATED 5 TIMES AND THEN 
ULTRASONICALLY CLEANED FOR 1/2 MINUTE. INSPECT FOR LOOSE, CRUSHED OR MISALIGNMENT 
OF CONTACTS. 


© THIS SHEET ADDED 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES ,N 

TOLERANCES ON * pwg mo 

FRACTIONS DECIMALS ANGLES drawn 
±. ±. dt 

CHECKE 

DO NOT SCALE THIS DRAWING APPROV 

MATERIAL APPROV 

AS SHOWN 


PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAB 
Camwiogi. Mam. 


NOMENCLATURE OR FIND 

DESCRIPTION NO. 

LIST OF MATERIALS 

MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 

CONNECTOR ELECTRICAL 

37 CONTACTS PLUG $ RECEPTACLE 

SPECFICATION CONTROL DRAWING 


APPLICATION 


HEAT TREATMENT 

FINAL FINISH 

AS SHOWN 


NASA APPROVAL^ 


MIT APPROVAL 


CODE IDENT NO. SIZE 


NASA DRAWING NO. 

1001498 


WM9 4 


|SHEET 2 OF 3 


1498 - 





























3 


2 




86171001 


REVISIONS 


DESCRIPTION 


-MOUA/r/A /6 PIAS£ 


\ 


LAAAA f£A/CAASL/LAr££>) 


X££ SA££X / £0*/&T/S-AWS _ 

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PER TDRR - — 

REVISED PER TDRR teals' -)klljA kMl 


NO 2-56NC-2A 

■cAAr/yx xcaxxv 


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PART OR 
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Cammibos. Mam. 


AS SHOWN 



NOMENCLATURE OR 
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LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


COm£Cr&P r £l£CTP/CJl 

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CODE IDENT NO. SIZE 



1001498 


SHEET 3 Of J 


APPLICATION 

















































































os,a, ... 


NOTICE — WHEN COVERNMCNT DRAWINGS. tPECIFICATION*. 0« OTHER DATE 
ARE USED FOR ANT PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELT 
RELATED COVERNNENT PROCURENENT OPERATION. THE UNITED STATES COVERN- 
NENT THERERT INCURS NO RESPONSIRILITY NOR ANT OCLICATION WHATSOEVER: 
AND THE FACT THAT THE COVERNNENT NAY HAVE FORMULATED. FURNISHED. OR 
IN ANT WAY SUPPLIEO THE SAID DRAWINCS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO RE RECARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSINC THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY- 
INC ANY RICHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL AMT 
PATENTED INVENTION THAT NAY IN ANT WAV BE RELATED THERETO. 


EEDCLKMENTCsr 

-^.^etNEWSE#'- 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. UNITS SHALL BE CAPABLE OF MEETING THE APPLICABLE REQUIREMENTS OF MIL-C-8384. EXCEPT AS 
AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

C. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND 1015404, CLASS 2. 
D UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED IN ND 1002052 

UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS SECTION (3) OF THIS DRAWING. 

E. PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001498). REVISION LETTER, DASH NUMBER 

THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING DATE 
OR CODE. UNITS SHALL BE INDIVIDUALLY PACKAGED PER ND 1002215, CLASS I 

F. MARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001498), REVISION 

LETTER AND DASH NUMBER SHALL BE MARKED ON THE UNIT PER ND 1002019. 


ACCEPTANCE AND INSPECTION 
DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 900 VOLTS RMS MINIMUM PER METHOD 301 OF MIL-STD-202 

INSULATION RESISTANCE: 200K MEGOHMS, MINIMUM AT 500 VOLTS DC PER METHOD 302 OF MIL-STD-202. 

DIMENSIONS AS SPECIFIED HEREIN. . , ' 

100X INSPECTION: INSPECT OPTICALLY FOR EVIDENCE OF CRACKS, BURRS, LOOSE CONTACTS, 

CONTACT ALIGNMENT, VOIDS, FLAWS OR ANY FOREIGN MATTER DETRIMENTAL TO THE FUNCTION OF ■'* 

THE CONNECTOR. CONTACT MATING SURFACES SHALL BE FREE FROM CRACKS, BURRS, BENDS AND 
FOREIGN PARTICLES. 


DESIGN REQUIREMENTS: 

MAXIMUM WORKING VOLTAGE: 250 VOLTS DC, 175 VOLTS RMS. 

DIELECTRIC WITHSTANDING VOLTAGE: 100,000 FEET: 250 VOLTS RMS. PER METHOD 301 OF MIL-STD-202 
CURRENT RATING: 3 AMPERES RMS, MAXIMUM 

CONTACT VOLTAGE DROP: 25 MILLIVOLTS, MAXIMUM AT 3 AMPERES DC. 

INSERTION AND WITHDRAWAL: (WITH MATING CONNECTOR) INDIVIDUAL CONTACTS SHALL ' . 

HAVE A MAXIMUM ENGAGEMENT FORCE OF 6 OUNCES AND A MINIMUM WITHDRAWAL FORCE OF 
5 OUNCES. ASSEMBLIES SHALL NOT EXCEED A MATING FORCE EQUAL TO THE PRODUCT OF 
THE NUMBER OF CONTACTS X 7.5 OUNCES OR BE lESS THAN A MINIMUM WITHDRAWAL FORCE EQUAL TO THE PRODUCT 

CONTAC^UFE* ^FTER^O^CYCLE^OF ENGAGEMENT AND DISENGAGEMENT OF THE CONNECTORS’AT 120 CYCLES/HOUR MAX, 
THE CONTACT VOLTAGE DROP SHALL BE 35 MV AT 3 ADC AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 
DIELECTRIC MATERIAL: (BODY) DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-19833, GDI-30. 

LEADS: SHALL BE 28 STRANDED WIRE. TEFLON INSULATED, PER MIL-W-16878. TYPE ET. 

COLOR CODED PER TABLE I. , , 

(1) LEADS SHALL WITHSTAND A 4 LB AXIAL PULL (APPLIED GRADUALLY)FOR 10 SECONDS. 

CAPTIVE SCREW- CRES TYPE 303 PER MIL-S-7720, PASSIVATED PER FINISH 5.4.2 OF MIL-STD-171 
MOUNTING PLATE: BRASS, TIN PLATED PER MIL-T t 10727, TYPE I, FUSED OVER COPPER FLASH. 

STUD- STEEL TIN PLATED PER MlL-T-10727,’WE I, FUSED OVER COPPER FLASH. INTERNAL THREADS TO 
BE FREE OF ELECTRO-TIN ELATING. STUD SHALL BE FASTENED SECURELY AND HERMETICALLY SEALED 
TO MOUNTING PLATE. 


REVISIONS 


DATE I APPROVAL 


- V © 


REPLACES SHEET I REV B I-/.//I,*/ 
WITH CHANGES lOf 7$ Y'/fM 


REVISED PER TDRR WI4I 


I 


REPLACES SHEET 1 REV B WITH CHANGES 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


M I T 

INSTRUMENTATION LAB 
Cammiooc. Mam. 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND 1002034 FOR THIS DRAWING 


UNLESS OTHERWISE SPECIFIED M 1 

DIMENSIONS ARE IN INCHES >NSTf ^^.M 

TOLERANCES ON —. bo. 

FRACTIONS DECIMALS ANGLES drawn ~T'H&aJO 

± ± ± CHECKED -£LJ2hl 

DO NOT SCALE THIS DRAWING APPROVAL 

SERIAL iDoonvii jdA* 

AS SHOWN APPROVAL 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 

CONNECTOR ELECTRICAL 

37 CONTACTS PLUG $ RECEPTACLE 

SPECIFICATION CONTROL DRAWING 


| HEAT TREATMENT 


I FINAL FINISH 


APPLICATION 


AS SHOWN 


NASA APPROVAL i 


MIT APPROVALS 


| CODE IDENT NO. I SIZE 


NASA DRAWING NO. 

1001498 


I SHEET I or 3 



■PHOTOGRAPHIC 8CALE OHET 




















3 


2 


NOTICE — WHEN GOVERNMENT DRAWINGS. SPECIFICATIONS. OR OTHER DATA 
ARE USED FOR ANT PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
RELATED SOVERNNENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN¬ 
MENT THEREBY INCURS NO RESPONSIBILITY NOR ANY OBLIGATION WHATSOEVER: 
AND THE FACT THAT THE GOVERNMENT MAY HAVE FORMULATED. FURNISHED. OR 
IN ANY WAY SUPPLIEO THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO BE REGARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSING THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY¬ 
ING ANY RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL AMY 
PATENTED INVENTION THAT MAY IN ANY WAY BE RELATED THERETO. 


L. VIBRATION: DURING VIBRATION PER ND 1002052, DISCONTINUNITY SHALL BE 0.1 MICROSECOND 

■ .* OR LESS, AT 100 MA DC FOR MATED CONNECTORS. , uflTrn dbibo 

M. CONTACT RESISTANCE: 10 MILL I OHMS MR* AT 100 MADC TEST PER MIL-STD-202, METHOD 307. (MATED PAIRS) 

N. TEMPERATURE OPERATING: -55°C TO ♦150 # C. 


SPECIAL REQUIREMENTS: (BY SUPPLIER) 

CONTACT SEPARATION: (100%'INSPECTION) ALL PIN CONTACTS SHALLBE TESTED WITH A 
STEEL TEST SLEEVE HAVING AN INSIDE DIAMETER OF .0230 F ^ 

MICRO-INCHES MAX. THE TOTAL WEIGHT OF THE tCSf SLEEVE SHALL BE .5 OUNCES 

WHEN THE ASSEMBLY IS INVERTED THE PIN CONTACT SHALL RETAIN THE .5 OUNCE WEIGHT. 

THIS TEST SHALL BE PERFORMED SEQUENTIALLY ON EACH CONTACT AFTER ASSEMBLY MlTH THE CONNECTOR BODY. 

THE FOLLOWING LOT SAMPLE TESTS SHALL BE MADE PRIOR TO 

shipment: 

(1) TENSILE STRENGTH: 

THE CRIMPED ASSEMBLIES FROM EACH TOOL SHALL BE SAMPLED PER MIL-STD-414 

INSPECTION LEVEL IV, AQL .4. THE ASSEMBLIES SHALL BE TESTED ON A HUNTER SCALE (OR EQUIVALENT) 
FOR TENSILE STRENGTH AND THE READINGS SHALL BE RECORDED. ALL ASSEMBLIES 
SHALL BE WITHIN THE CONTROL LIMITS STATED BELOW OR THE LOT SHALL BE 
REJECTED. ASSEMBLIES SHALL BE PACKAGED AND IDENTIFIED WITH THE LOT NUMBER, 

WHICH SHALL ACCOMPANY THE UNITS TO FINAL INSPECTION, AND BE INCLUDED WITH 
THE CONNECTOR SHIPMENT. THIS APPLIES TO BOTH PINS AND SOCKETS. 

THERE SHALL BE TWO DATA SHEETS FOR THE CRIMPING OF THE PINS, ONE FOR THE PIN END 

and one for the wire end, 


a I 86171001 


REVISIONS 


to irr 


DESCRIPTION 


THIS SHEET ADDED PER 
TO R % lO ? 7S' _ 

REVISED PER TDRRIII4I 


u>H 


CONTACT 
END (Ml 
3.0 LBS 


4.0 LBS 


SOCKET 


4.0 LBS 


(?) SOCKET STRENGTH, SIDE LOAD (IN CONNECTOR): 18 OUNCES MINIMUM SHALL BE APPLIED AT 
THE PIN ENGAGING END OF THE SOCKET. INTERMATABIL1TY AND PERFORMANCE SHALL NOT BE 
IMPAIRED 

V MATING AND CLEANING: (lOO% INSPECTION) EACH CONNECTOR SHALL BE MATED 5 TIMES AND THEN 
ULTRASONICALLY CLEANED FOR 1/2 MINUTE. INSPECT FOR LOOSE, CRUSHED OR MISALIGNMENT 
OF CONTACTS. 


© THIS SHEET ADDED 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
± ± ± 

DO NOT SCALE THIS DRAWING 
MATERIAL 

AS SHOWN 


PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAB 
Cam win doc. Mam. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 

CONNECTOR ELECTRICAL 

37 CONTACTS PLUG $ RECEPTACLE 

SPECIFICATION CONTROL DRAWING 


I HEAT TREATMENT 


I FINAL FINISH 


APPLICATION 


AS SHOWN 


NASA APPROVAL^ 


MIT APPROVAL v 


I CODE IDENT NO. SIZE 


NASA DRAWING NO. 

IOOI498 


2 OF S 






















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PART OR 
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UNLESS OTHERWISE SPECIFIED 
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TOLERANCES ON 
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-±. •— ^.004 

Z CHECKED 

DO NOT SCALE THIS DRAWING APPROVAL 

MATERIAL ■ 

AS SHOWN 


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INSTRUMENTATION LAB 
Cambridm. Mam. 

contract 


DATE ^2^ 


APPROVAL 

a& 




APPLICATION 


HEAT TREATMENT 


FINAL FINISH 

AS SHOWN 



NOMENCLATURE OR 
DESCRIPTION 

LIST OF MATERIALS _ 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


COM£Croe, £l£CTX/C*l 
J7 co/vrAcrs, / **crryxccz* 

srsc/rycsr/## c/xy^oz **A»/Avr 


CODE IDENT NO. SIZE NASA DRAWING NO. 

C 1001498 















































3 


NOTICE — WHEN GOVERNMENT DRAWINGS. SPECIFICATIONS. OR OTHER DATA 
ARE USED FOR ANY PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
RELATED GOVERNMENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN¬ 
MENT THEREBY INCURS NO RESPONSIBILITY NOR ANY OBLIGATION WHATSOEVER; 
AND THE FACT THAT THE GOVERNMENT MAY HAVE FORMULATED. FURNISHED. OR 
IN ANY WAY SUPPLIED THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO BE REGARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSING THE HOLOER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY¬ 
ING ANY RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL AMY 
PATENTED INVENTION THAT MAY IN ANY WAV BE RELATED THERETO. 


REQUIREMENT Sir-' • 

v .^ 6g H E R <g 

A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. UNITS SHALL BE CAPABLE OF MEETING THE APPLICABLE REQUIREMENTS OF MIL-C-8384. EXCEPT AS 
AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

C. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND 1015404, CLASS 2. 

D. UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED IN ND 1002052 
UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS SECTION (3) OF THIS DRAWING. 

E. PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001498). REVISION LETTER, DASH NUMBER 

THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING DATE 
OR CODE. UNITS SHALL BE INDIVIDUALLY PACKAGED PER ND 1002215, CLASS I 

F. MARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001498), REVISION 

LETTER AND DASH NUMBER SHALL BE MARKED ON THE UNIT PER ND 1002019. 


ACCEPTANCE AND INSPECTION 
DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 900 VOLTS RMS MINIMUM PER METHOD 301 OF MIL-STD-202 

INSULATION RESISTANCE: 200K MEGOHMS. MINIMUM AT 500 VOLTS DC PER METHOD 302 OF MIL-STD-202. 

DIMENSIONS AS SPECIFIED HEREIN. 

100% INSPECTION: INSPECT OPTICALLY 10 X MAGNIFICATION FOR EVIDENCE OF CRACKS, BURRS^LOOSE CONTACTS, 
CONTACT ALIGNMENT, VOIDS, FLAWS OR ANY FOREIGN MATTER DETRIMENTAL TO THE FUNCTION OF 
THE CONNECTOR. CONTACT MATING SURFACES SHALL BE FREE FROM CRACKS, BURRS, BENDS AND 
FOREIGN PARTICLES. 


3. . DESIGN REQUIREMENTS: 

A. MAXIMUM WORKING VOLTAGE: 250 VOLTS DC, 175 VOLTS RMS. 

B. DIELECTRIC WITHSTANDING VOLTAGE: 100,000 FEET: 250 VOLTS RMS. PER METHOD 301 OF MIL-STD-202 

C. CURRENT RATING: 3 AMPERES RMS, MAXIMUM 

D. CONTACT VOLTAGE DROP: 25 MILLIVOLTS, MAXIMUM AT 3 AMPERES DC. 

E. INSERTION AND WITHDRAWAL: (WITH MATING CONNECTOR) INDIVIDUAL CONTACTS SHALL 
HAVE A MAXIMUM ENGAGEMENT FORCE OF 6 OUNCES AND A MINIMUM WITHDRAWAL FORCE OF 
.5 OUNCES. ASSEMBLIES SHALL NOT EXCEED A MATING FORCE EQUAL TO THE PRODUCT OF 

THE NUMBER OF CONTACTS X 7.5 OUNCES OR BE LESS THAN A MINIMUM WITHDRAWAL FORCE EQUAL TO THE PRODUCT 
OF THE NUMBER OF CONTACTS X 1 OUNCE.INITIALLY - 0.5 OUNCES AFTER LIFE 

F. CONTACT LIFE: AFTER 500 CYCLES OF ENGAGEMENT AND DISENGAGEMENT OF THE CONNECTORS AT 120 CYCLES/HOUR MAX, 
THE CONTACT VOLTAGE DROP SHALL BE 35 MV AT 3 ADC AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. 

G. DIELECTRIC MATERIAL: (BODY) DIALLYL PHTHALATE, GLASS FILLED PER MIL-M-19833, GDI-30. 

H. LEADS: SHALL BE 28 STRANDED WIRE, TEFLON INSULATED. PER MIL-W-16878.• TYPE ET, 

COLOR CODED PER TABLE I. 

(1) LEADS SHALL WITHSTAND A 4 LB AXIAL PULL (APPLIED GRADUALLY)FOR 10 SECONDS. 

I. CAPTIVE SCREW: CRES TYPE 303 PER MIL-S-7720, PASSIVATED PER FINISH 5.4.2 OF MIL-STD-171 

J. MOUNTING PLATE: BRASS, TIN PLATED PER MIL-Tr10727, TYPE I, FUSED OVER COPPER FLASH. 

K. STUD: STEEL, TIN PLATED PER MIL-T-10727, TYPE l, FUSED OVER COPPER FLASH. INTERNAL THREADS TO 
BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENED SECURELY AND HERMETICALLY SEALED 

TO MOUNTING PLATE. 


REVISIONS 

IYM DESCRIPTION 

C REPLACES SHEET I REV B 
WITH CHANGES IO?7& 

D REVISED PER TDRR 14141 
E REVISED PER TDPR 11997_ 

F REVISED PER TDRR 14792 


\m4\uM 


REPLACES SHEET 1 REV B WITH CHANGES 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


UNLESS OTHERWISE SPECIFIED M 1 T 

DIMENSIONS ARE IN INCHES INSTRUMENTATION LAB 

TOLERANCES ON pw«, »o. comtbact 

FRACTIONS DECIMALS ANGLES drawn 'TftBUO date 

“ CHECKED Ol' > 

DO NOT SCALE THIS DRAWING APPPnvAi fifty. 

“"""as shown 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND 1002034 FOR THIS DRAWING 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 

CONNECTOR ELECTRICAL 

37 CONTACTS PLUG $ RECEPTACLE 

SPECIFICATION CONTROL DRAWING 


HEAT TREATMENT 


NASA APPROVAL/ 


(FINAL FINISH 


APPLICATION 


AS SHOWN 


MIT APPROVAL 




^ CODE IDENT NO. SIZE 

;_c 

- SCALE - WT 


NASA DRAWING NO. 

1001498 


SHEET I OF 3 
















- NOTICE — WHEN GOVERNMENT DRAWINGS. SPECIFICATIONS. ON OTHER DATA 
ARE USED TOR ANT PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
RELATED GOVERNMENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN¬ 
MENT THEREBY INCURS NO RESPONSIBILITY NOR ANY OBLIGATION WHATSOEVER; 
ANO THE FACT THAT THE GOVERNMENT MAY HAVE FORMULATED. FURNISHED. OR 
IN ANY WAY SUPPLIED THE SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO RE REGAROED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 
| LICENSING THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY. 
I ING ANY RIGHTS OR PERMISSION TO MANUFACTURE. USE. OR SILL AMY 
I PATENTED INVENTION THAT MAY IN ANY WAY BE RELATED THERETO. 


d 86171001 


REVISIONS 

DESCRIPTION _ 

THIS SHEET ADDED P£R 

TDRR toils' _ 

REVISED PER TORR III4I 

REVISED PER TDRR 11997- _ 

REVISED PER TORR 14792 


IQjlf 


lot 


L. VIBRATION: DURING VIBRATION PER ND 1002052, 01SC0NTINUNITY SHALL BE 0.1 MICROSECOND 
* OR LESS, AT 100 MA DC FOR MATEO CONNECTORS. 

M. CONTACT RESISTANCE: 10 MILLIOHMS HA* AT 100 MADC TEST PER MIL-STD-202, METHOD 307. (MATED PAIRS) 

N. TEMPERATURE OPERATING: -55°C TO +150°C. 


SPECIAL REQUIREMENTS: (BY SUPPLIER) 

CONTACT SEPARATION: (100%‘INSPECTION) ALL PIN CONTACTS SHALLBE TESTED WITH A 
STEEL TEST SLEEVE HAVING AN INSIDE DIAMETER OF .0230 AND FINISH OF 16 

MICRO-INCHES MAX. THE TOTAL WEIGHT OF THE TESf SLEEVE SHALL BE .5 OUNCES . 

WHEN THE ASSEMBLY IS INVERTED THE PIN CONTACT SHALL RETAIN THE .5 OUNCE WEIGHT. 

THIS TEST SHALL BE PERFORMED SEQUENTIALLY ON EACH CONTACT AFTER ASSEMBLY WITH THE CONNECTOR BODY. 

THE FOLLOWING LOT SAMPLE TESTS SHALL BE MADE PRIOR TO 

SHIPMENT: 

(1) TENSILE STRENGTH: 

THE CRIMPED ASSEMBLIES FROM EACH TOOL SHALL BE SAMPLED PER MIL-STD-414 

INSPECTION LEVEL IV, AQL .4. THE ASSEMBLIES SHALL BE TESTED ON A HUNTER SCALE (OR EQUIVALENT) 
FOR TENSILE STRENGTH AND THE READINGS SHALL BE RECORDED. ALL ASSEMBLIES 
SHALL BE WITHIN THE CONTROL LIMITS STATED BELOW OR THE LOT SHALL BE 
REJECTED. ASSEMBLIES SHALL BE PACKAGED AND IDENTIFIED WITH THE LOT NUMBER, 

WHICH SHALL ACCOMPANY THE UNITS TO FINAL INSPECTION, AND BE INCLUDED WITH 
THE CONNECTOR SHIPMENT. THIS APPLIES TO BOTH PINS AND SOCKETS. 

THERE SHALL BE TWO DATA SHEETS FOR THE CRIMPING OF THE PINS, ONE FOR THE PIN END 
AND ONE FOR THE WIRE END, 


CONTACT 

END 


SOCKET 


3.0 LBS 


4.0 LBS 


4.0 LBS 


(2) SOCKET STRENGTH, SIDE LOAD (IN CONNECTOR): 18 OUNCES MINIMUM SHALL BE APPLIED AT 
THE PIN ENGAGING END OF THE SOCKET. INTERMATABILITY AND PERFORMANCE SHALL NOT BE 
IMPAIRED. 

MATING AND CLEANING: (lOO% INSPECTION) EACH CONNECTOR SHALL BE MATED 5 TIMES AND THEN 
ULTRASONICALLY CLEANED FOR 1/2 MINUTE. INSPECT FOR LOOSE, CRUSHED OR MISALIGNMENT 
OF CONTACTS. 


© THIS SHEET ADDED 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 
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| NASA APPROVAL a 


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.DATE_ 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 

CONNECTOR ELECTRICAL 

37 CONTACTS PLUG $ RECEPTACLE 

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I CODE IDENT NO. SIZE 



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C 1001498 


SCALE - WT SHEET 3 OF J 


1 










































































notice — WHEN 60VERNMENT DMWINtt. SPECIFICATIONS. ON OTHER DATA 
ARE USED FOR ANT PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY; 
RELATED COVERNNENT PROCURENENT OPERATION. THE UNITED STATES 60VERN- 
NENT THEREBY INCURS NO RESPONSIBILITY NOR ANY ORLISATION WHATSOEVER; 
AND THE FACT T"M THE SOVERNNENT MAY HA IS FORNULATED. FURNISHED. OR 
IN ANY WAV SUPPLIED THE SAID DRAWINCS. SPECIFICATIONS OR OTHER DATA IS 
NOT TO BE RE6ARDED BY INPLICATION OR OTHERWISE AS IN ANY MANNER 
LICENSING THE HOLDER OR ANY OTNER PERSON OR CORPORATION. OR CONVEY- 
INS ANY RI6HTS OR PERMISSION TO MANUFACTURE. USE. OR SELL ANY 
PATENTED INVENTION THAT MAY IN ANY WAV BE RELATED THERETO. 


' ' " v -m ' 

|^B3gl»affWTfe^ v * 

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A. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

B. UNITS SHALL BE CAPABLE OF MEETING THE APPLICABLE REQUIREMENTS OF MIL-C-8384. EXCEPT AS 
AND IN ADDITION TO THE REQUIREMENTS SPECIFIED HEREIN. 

C. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS SPECIFIED IN ND 1015404, CLASS 2. 

D. UNITS SHALL BE CAPABLE OF MEETING ALL QUALIFICATION REQUIREMENTS SPECIFIED IN ND 1002052 
UNLESS MODIFIED OR AMMENDED BY THE DESIGN REQUIREMENTS SECTION (3) OF THIS DRAWING. 

E. PACKAGING AND PACKING: UNIT PACKAGES AND EXTERIOR SHIPPING CONTAINERS SHALL BE 
MARKED WITH THE DRAWING NUMBER (1001498). REVISION LETTER, DASH NUMBER 
THE MANUFACTURER'S NAME OR SYMBOL, LOT OR SERIAL NUMBER AND THE MANUFACTURING DATE 
OR CODE. UNITS SHALL BE INDIVIDUALLY PACKAGED PER ND 1002215, CLASS I 

F. MARKING: THE MANUFACTURER'S NAME OR SYMBOL, DRAWING NUMBER (1001498), REVISION 

LETTER AND DASH NUMBER SHALL BE MARKED ON THE.UNIT PER ND 1002019. 


y ybviuui 


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DESCRIPTION 

DATE 

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2.V 

A. 


B. 

C. 

D. 


ACCEPTANCE AND INSPECTION 


DIELECTRIC WITHSTANDING VOLTAGE: 

(1) SEA LEVEL: 900 VOLTS RMS MINIMUM PER METHOD 301 OF MIL-STD-202 

INSULATION RESISTANCE: 200K MEGOHMS, MINIMUM AT 500 VOLTS DC PER METHOD 302 OF MIL-STD-202. 


DIMENSIONS AS SPECIFIED HEREIN. _ 

100% INSPECTION: INSPECT OPTICALLY 10 X MAGNIFICATION FOR EVIDENCE OF CRACKS, BURRS,LOOSE CONTACTS^ 
CONTACT ALIGNMENT, VOIDS, FLAWS OR ANY FOREIGN MATTER DETRIMENTAL TO THE FUNCTION OF 
THE CONNECTOR. CONTACT MATING SURFACES SHALL BE FREE FROM CRACKS, BURRS, BENDS AND 
FOREIGN PARTICLES. 




DESIGN REQUIREMENTS: 


A. 

B. 

C. 

D. 

E. 


MAXIMUM WORKING VOLTAGE: 250 VOLTS DC, 175 VOLTS RMS. 

DIELECTRIC WITHSTANDING VOLTAGE: 100,000 FEET: 250 VOLTS RMS. PER METHOD 301 OF MIL-STD-202 

CURRENT RATING: 3 AMPERES RMS, MAXIMUM ' 

CONTACT VOLTAGE DROP: 25 MILLIVOLTS. MAXIMUM AT 3 AMPERES DC. 

INSERTION AND WITHDRAWAL: (WITH MATING CONNECTOR) INDIVIDUAL CONTACTS SHALL ‘ - 

HAVE A MAXIMUM ENGAGEMENT FORCE OF 6 OUNCES AND A MINIMUM WITHDRAWAL FORCE OF 
5 OUNCES. ASSEMBLIES SHALL NOT EXCEED A MATING FORCE EQUAL TO THE PRODUCT OF 
THE NUMBER OF CONTACTS X 7.5 OUNCES OR BE LESS THAN A MINIMUM WITHDRAWAL FORCE EQUAL TO THE PRODUCT 

'StSSr-TSS? D.iSSmSToV the connectors ^ © REPLACES SHEET 1 REV B WITH CHANGES 

THE CONTACT VOLTAGE DROP SHALL BE 35 MV AT 3 ADC AND THE INSERTION AND WITHDRAWAL FORCE SHALL BE AS SPECIFIED HEREIN. ^ 

DIELECTRIC MATERIAL: (BODY) DIALLYL PHTHALATE, GLASS FILLED PER MIL-M- 14 , TYPE SDG 
LEADS: SHALL BE 28 STRANDED WIRE, TEFLON INSULATED, PER MlL-W-16878. TYPE ET, 

COLOR CODED PER TABLE I. . 

(1) LEADS SHALL WITHSTAND A 4 LB AXIAL PULL (APPLIED GRADUALLY)FOR 10 SECONDS. . 

CAPTIVE SCREW: CRES TYPE 303 PER MIL-S-7720, PASSIVATED PER FINISH 5.4.2 OF MlL-STD-171 ■ ■ - . 

MOUNTING PLATE: BRASS, TIN PLATED PER MIL-T r 10727, TYPE I, FUSED OVER COPPER FLASH. 

STUD- STEEL TIN PLATED PEB MIL-T-10727. Wfts*. FUSED OVER COPPER FLASH. INTERNAL THREADS TO v 

BE FREE OF ELECTRO-TIN PLATING. STUD SHALL BE FASTENED SECURELY AMB HERMETICALLY SEALED 


TO MOUNTING PLATE. 


PROCURE ONLY FROM APPROVED SOURCES LISTED ON 
ND 1002034 FOR THIS DRAWING 














i 


next 'assy 

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NOTICE — WHEN GOVERNNENT DRAWINGS. SPECIFICATIONS. OR OTHER DATA 
ARE USED FOR ART RURROSE OTHER THAR IR CORRECTIOR WITH A DEFINITELY 
RELATED GOVERNNENT PROCUREMENT ORERATIOR. THE UNITED STATES GOVERN- 
RENT THEREBY <HCUR$ RO RESPONSIBILITY ROR ARY OBLIGATION WHATSOEVER; 
AND THE FACT 1HAT THE GOVENNNENT RAT HAVE FORMULATED, FURRISHED. OR 
IM ART WAT SURRLIEO THE SAID 0RAWIH6S. SRECIFICATIORS OR OTHER DATA IB 
ROT TO BE RECARDED BY IMPLICATION OR OTHERWISE ASINANY MANNER 
LICERSING THE HOLDER OR ARY OTHER PERSOH OR CORPORATOR. OR CORVEY- 
IRG ARY RIGHTS OR PERMISSIOH TO MARUFACTURE. USE. OR SELL ARY 
PATERTED IHVERTIOR THAT MAY IR ARY WAY BE RELATED THERETO. 


9 86171001 


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VIBRATION: DURING VIBRATION PER ND 1002052, DISCONTINUNITY SHALL BE 0.1 MICROSECOND 
OR LESS, AT 100 HA DC FOR HATED CONNECTORS. „„„„„ /M « TFn P aidc\ 

H. CONTACT RESISTANCE: 10 M ILL I OHMS «» AT 100 HADC TEST PER MIL-STD-202, METHOD 307. (MATEO PAIRS) 

N. TEMPERATURE OPERATING: -55°C TO +150°C. 


4. 


A. 


B. 


SPECIAL REQUIREMENTS: (BY SUPPLIER) 

CONTACT SEPARATION: (100X*INSPECTION) ALL PIN CONTACTS SHALLBE TESTED WtTH A 
STEEL TEST SLEEVE HAVING AN INSIDE DIAMETER OF .0230 +888o AND F ^ , 

MICRO-INCHES MAX. THE TOTAL WEIGHT OF THE YESfSLEEVE SHALL BE .5 OUNCES + -1 

WHEN THE RBSEMBLY IS INVERTED THE PIN CONTACT SHALL RETAIN THE .5 OUNCE WEIGHT. 

THIS TEST SHALL BE PERFORMED SEQUENTIALLY ON EACH CONTACT AFTER ASSEMBLY KITH THE CONNECTOR BODY. 

THE FOLLOWING LOT SAMPLE TESTS SHALL BE MADE PRIOR TO 

shipment: 

(1) TENSILE STRENGTH: ■ , 

THE CRIMPED ASSEMBLIES FROM EACH TOOL SHALL BE SAMPLED PER MIL-STD-414 

INSPECTION LEVEL IV, AQL .4. THE ASSEMBLIES SHALL BE TESTED ON A HUNTER SCALE (OR EQUIVALENT) 
FOR TENSILE STRENGTH AND THE READINGS SHALL BE RECORDED. ALL ASSEMBLIES 
SHALL BE WITHIN THE CONTROL LIMITS STATED BELOW OR THE LOT SHALL BE 
REJECTED. ASSEMBLIES SHALL BE PACKAGED AND. IDENTIFIED WITH THE LOT NUMBER, 

WHICH SHALL ACCOMPANY THE UNITS TO FINAL INSPECTION, AND BE INCLUDED WITH 
THE CONNECTOR SHIPMENT. THIS APPLIES TO BOTH PINS AND SOCKETS. 

THERE SHALL BE TWO DATA SHEETS FOR THE CRIMPING OF THE PINS, ONE FOR THE PIN END 
AND ONE FOR THE WIRE END, 



PIN 

SOCKET 

WIRE 

SIZE 

CONTACT 

END (MIN) 

WIRE 

END (MIN) 

WIRE 

END (MIN) 

’ 28 

3.0 LBS 1 

4.0 LBS 

4.0 LBS 


(z) SOCKET STRENGTH, SIDE LOAD (IN CONNECTOR): 18 OUNCES MINIMUM SHALL BE APPLIED AT 
THE PIN ENGAGING END OF THE SOCKET. INTERMATABILITY AND PERFORMANCE SHALL NOT BE 

MATING AND CLEANING: (lOO% INSPECTION) EACH CONNECTOR SHALL BE MATED 5 TIMES AND THEN 

ULTRASONICALLY CLEANED FOR 1/2 MINUTE. INSPECT FOR LOOSE, CRUSHED OR MISALIGNMENT . 

OF CONTACTS. 


© THIS SHEET ADDED 


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M I T 

INSTRUMENTATION LAB 
Cambridm. Maw. 

G. NO. _CONTRACT 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


DRAWN THStiO __ DATE 
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CONNECTOR ELECTRICAL 

37 CONTACTS PLUG $ RECEPTACLE 

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l 'AQjHT, BALAfJCE MlQ Gf/8AL 1000262 
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SEE NOTE I3j 4~8 
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EENQTE6 40 
EE NOTEC 39 
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DRAWING NUMBER | 

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STABLE 

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1001453-2 

' *. 

100438-3 


IC0I483-4 

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-OH,-021, 

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.166 f\ 

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typical installation 

SEE NOTE 9 


rSEE NOTES 



VIEW C-C 


NOTES 

L INTERPRET DRAWING M ACCORDANCE WITH ML-0-70327 
Z ASSEMBLE £ TEST PER REQUIREMENTS OF ATP . , ;• FTM u,0020i 
a SCREW TORQUE REQUIREMENTS ±7% 

A. IQO IN. LB. 

a 5.0 n. La 

C. ! .0 IN LB. 

Q8S.0 JN.LB 
E. 70.0 H LB 
E 65.0 IN LB 
G30.0 IMJI 


H. 3.5 IN. LB. 


A MARK CHARACTERS^HIGH COLOR BLACK PER NO 1002019 AT LOCATIONS SHOWN. 

FNGCA/E CHARACTERS -|J high AMO Fill. COLOR BLACK PER ISO 1002019 

- BALANCE \A€OHTS ano nuts to be selected from applicable drawings ano 
■mstalled per ATPIOOOOOI. SELECT SCREWS FROM CHART SEE \CTE 9 
USE DRAWING NUMBERS \ - - QMBAL ASSEMBLY OUTLINE AND 1000017 
/.RING DIAGRAM for reference 

PROTECTIVE COVER.EUECT.NASA DRAWING NO. 1001495, PROTECTIVE COVER, COOL ANT, 

NASA DRAWING NO. 1001494, MOUNTING PAD COVERS, NASA DRAWING NO:S OOI4GO,10<3l464<1001461 

aSeN^^UiS^JRiNG^ TK^^ I |!^l1^tIoI^?^PR0^ 0 h?aTER C PoS^R JLY 

TO INERT A u COMPONENTS. . SE SElF LOCKING SCREWS, NAS 35C04LL4,0R EQUIV, 

TC SECURE 1001495 TO CONNECTOR MOUNT. ASSY'S(T)Atort)SCREWS NOT TO PROJECT BELOW 
. . ,TtNG SURFACE ONI 7 ;ft (q REVOKE PROTECTIVECQVEP 

mounting screws and cable immediately prior to installation 

.►CURE BALANCE WEIGHTS.ITEMS (3?)THRU(40)TO GIMBALS WITH SCREWS PER 
TP FCTION CHART,ft (96 s nc?/^3)AT REQUIRED LOCATIONS ON MCOLE AND OJTPP 
MBALS.SEE VIEW E FOR TYPICAL INSTALLATION DATA, caution: do NOT INSTALL ITEM (56) OR 
TEM(?3)lN LOCATIONS THAT WILL PREVENT FREE ROTATION OF GIMBALS. 

'EMPERATURE OF ASSEMBLY • MUST BE MAINTAINED BETWEEN I20°F ANO I40 # E 
PULSED INTERGRATING PENDcL JM,NASA DRAWING NO. ■000013. MUST BE RECAl/BRATED 
IF TEVIPERaTJRE EXCEEDS t HESE LIMITS. GYRO PRFALIGNED ASSY.,NASA DRAWING NO. 

1000012 MUST BE RECALIBRATED IE TEMPERATURE EXCEEDS 40*F*T0 I60*F RANGE 
STAMP OR ENGRAVE SERIAL NUMBERS OF I RIGS. NASA DWG. NO. 1000012, AND PIPS NASA 
NC.IOOOOI3 IN APPROPRIATE BLOCKS PER NO 1002019 
"£V. O ^ ^3 BE SELECTED 8 MAINTAINED INCONJU\Z' 

' V EV (49) TO BE ASSEMBLED PER NASA 
S' EC* T EN (49) FROM TABLE I 

•* * ■ FFV? (46) 8 (37) TO ITEM(T)WITH ITEM (5§) COAT MATING SURFACES OF ( 46 )( 47 ) 8 CD 

* ■ r ‘-- f. W -E-ORE ASSEMBLY 

K -■ V PROCUREMENT . THIS ASST IMP MUST MEET THE -^L'REMENT OF PSlOOCZOI 

15 TAPE "E? 5- SHALL BE USED AS REQUIRED TC NIE-RtCT MOVEMENT OF THE HARNESS IN THE CABLE CLAMP 



16. COOLANT PASSAGES SHALL MEET THE CLEANLINESS REQUIREMENTS OF ND1002223 
WHEN ITEMS(^)j9])8(25)ARE ASSEMBLED TO CAS£,ITEM(T) 


'■ON WITH THIS ASSEMBLY. 

PAWINQ NO. 1007572 AT I.S.S. LEVEL. 


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12 


9 


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DRAWING number 

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04' !C5I 061 

C7 jCfi. 09 



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viewE 


3 5-MCNSS _11 007550-01: I 1007550-05! 

! 2 ,:^ NDS 1007550-02! 1007550-061 

; GRAPH MC _ 

2 S ^APHMC 1007550-03- ,007550-07. 

3 GPAP^MO ,1007550-041 IQQ7550-08I 

! -01,-021, 

IMJ CONFIGURAT ON! -031,-041 -071,-081,-091 
-051,-061 


TYPICAL INSTALLATION 
SEE NOTE 9 


|I007550-C4|T1007550 - O0IJ 


SEE NOTE & 





VIEW C-C 


MARK J3- 
SEE VIEW C-C 


NOES 

L INTERPRET DRAWING IN ACCORDANCE \MTh ML-D-70327 
^ ASSEMBLE $ TEST PER REQU»EN€NTS OF ATP IOOOOO|£ FTM 1000201 
3L SCREW TORQUE REQUIREMENTS t7% 

A. IQO MLB. 
a 5.o m i_a 
C. i .0 M LB 
QftxO MLB 
E. 70.(7 M LB 
c . 65.0 MLB 

a 3 o.o mlb 

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4 MARK CHARACTERS ^ 7 hiigh COLOR BLACK PER NO I002CH9 AT LOCATIONS SHOWN. 

5 ENGP/UE CHARACTERS $ HIGH ANO FILL. COLOR BLACK PER NO >002019 

- BALANCE \AOjHTS ANO NUTS TO BE SELECTED FROM APPLICABLE DRAWINGS AND 
INSTALLED PER ATPlOOCOOl. SELECT SCREWS FROM CHART SEE NOTE 9 
USE DRAWING NUMBERS 1000013 GIMBAL ASSEMBLY OUTLINE Af® 1000017 
//RING DIAGRAM FOR REFERENCE 

PROTECTIVE C0VER.EL£CT,NASA DRAWING NO. 1001495, PROTECTIVE COVER .COOLANT. 

NASA DRAWING NO. 100494, MOUNTING PAD COVERS, NASA DRAWING NO.’S 00(460,1001464<1001461 

WHETsf’^UlRED^JRiNG TESTED^N^Lt^TI^O^fl^PRWlcJE -^atI^POWE^^ 

TO INERT A^ COMPONENTS. . SE SELF LOCKING SCREWS, NAS; 35C04LL4,0R EQUIV, 

T 0 SECURE 1001495 TO CONNECTOR MOUNT. ASSY*S(T)ANDfF)SCREWS NOT TO PROJECT BELOW 
MC-NTING SURFACE 0N( 7 ;8 (8 ^ RE '1 /E PROTECT IV ECOVER" 

MOUNTING SCREWS AND CABLE IMMEDIATELY PRIOR TO INSTALLATION 
r SECURE BALANCE WEIGHTS.ITEMS (3E)THRu(40) TO GIMBALS WITH SCREWS PER 
SELECTION CHART ,8 (56 09(43) AT REQUIRED LOCATIONS ON MCOLE AND OUTER 
GIMBALS. SEE VIEW E FOR TYPICAL INSTALLATION DATA. CAUTION: DO NOT INSTALL ITEM (56) OR 
ITEM(43) IN LOCATIONS THAT WILL PREVENT FREE ROTATION OF GIMBALS. 

TEMPERATURE OF ASSEMBLY • MUST BE MAINTAINED BETWEEN I 20 °F ANO I40*E 
PULSED INTFRGRATiNG PEND^UM,NASA ORAWING NO.IOOOC13. MUST BE RECALIBRATED 
IF TEMPERATURE EXCEEDS T HESE LlMiTS. GYRO PREALIGNED ASSY.,NASA DRAWING NO. 

1000012 MUST BE RECAUBRAIED IF TEMPERATURE EXCEEDS 40*F*T0 IGOV RANGE 
STAM= OR ENGRAVE SERIAL NUMBERS OF I RIGS, NASA DWG. NCX KX)OOI2,ANO PIPS NASA 
NOIOOOOI3 |\ APPROPRIATE BlOCKS PER NO 1002019 

12. ITEM ® 0E SELECTED 8 VAIH ’A NED IN CONJUNCTION WITH THIS ASSEMBLY. 

iTEV (49) TO0E ASSEMBLED PER NASA DRAWING NO. 1007572 AT I.S.S. LEVEL. 

SELECT ITEM (49) FROM TABLE I 

13. BOND ITEMS (46) 8 (37) TO lTEM r T)wiTH ITEM (Jg). COAT MATING SURFACES OF (46)(47) 8CD 
WITH (48) BEFORE ASSEMBLY 

14. rr K •'ARES PROCLKUv.nMT ~H\S ASSEMBLY MUST MEET THE REQUIREMENT OF PSlOOCEOV 

15. TAPE ITEM (54, SHALL BE USED AS REQUIRED TO RESTRICT MOVEMENT OF THE HARNESS IN THE CABLE CLAMP 


HJZ) 

SEE NOTE 3F 


-M«K J2 
SEE MEW C-C TYP 





SEE VCW C-C TYP 



5 E NOTE ^ 

6 PLACES 


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r fCvJ t »€'- SC*N-fc ' • *5\. v TfCf •* 


«. COOLANT PASSAGES SHALL MEET THE CLEANLINESS REQUIREMENTS OF ND1002223 
WHEN ITEMSARE ASSEMBLED TO CASE,ITEM (T) 

17. APPLY SEALING COMPOUND PER NASA DRAWING NQ 1006338-000 70 SECURE 
PRECISION RESOLVER ADJUST POT SCREW HEADS SUBSEQUENT TO IS5 
LEVEL ADJUSTMENT. 








9 































































































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11007550-021 1007550-061 


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SEE NOTE 9 


23RAPHM0 1007550-021 1007550*071 

3 GRAPmMO *1007550-041 1007550 081 

-Oil. -021, 

IMU CONFIGURATE -031,-041 -07I.-06I.-C3I 
__; -05!,-061_ 


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MARK J! 
SEE VEW C-C 


NOTFS 

l WTERPRET ORAWNG N ACOORWNCE VMM ML-0-70327 
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C IjO RILR 
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4 MARK CHARACTERS^HIGH COLOR BLACK PER NO 1002019 AT LOCATIONS SHOWN. 

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f BALANCE WEIGHTS ANO NUTS TO BE SELECTED FROM APPLICABLE DRAWINGS ANO 
INSTALLED PER ATPlOOOOOL SELECT SCREWS FROM CHART SEE NOTE 9 
- USE DRAWING NUMBERS IQOOOtfc GlMBAL ASSEMBLY OUTLIC AMD 1000017 
WRING DIAGRAM POP REFERENCE 

r PROTECTIVE cnvFR.El_ECT.NASA OPAWING ND. 100*95, PROTECTIVE COYER .COOLANT, 

NASA DRAWING NO. 001494,mounting PAO COVERS, NASA DR4WNG NO'S Ob*6Q,1001464<KXX4«| 
lOOtd^AN&^iftf^SNPPKj W fFt ftTffft~OHfrmN O NO BO Cl t C Q TO be REMOVED ONLY 
WHEN REQUIRED DURING TEST AND INSTALLATION,OR TO PROVicfc HEATER POWER 
TO INERT Ak COMPONENTS. JSE SELF LOCKING SCREWS. NAS; 35C04LL4.0R EQUIV, 

TO SECURE 1001495 TC C0NN6CT0R MOUNT. ASSTS(T)AM)(T)SCRE\AS NOT TO PRoicT BELOW 
MOwNTMG SURFACE ONCtJS (62 REVIVE PROTECT IVETOVEK 
MOUNTING SCREWS AND CABLE IMMEDIATELY PRIOR TO INSTALLATION 
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..TEMPERATURE Of ASSEMBLY MUST BE MAINTAINED BETWEEN 120*F AND I40*E 
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IF TEMPERATURE EXCEEDS t hESE LIMITS GYRO PRFALIGNED ASSY.,NASA QRAWW6 NO. 

1000012 MUST BE RECAUBRAfED f TEMPERATURE EXCEEDS AOVTO lGO*F RANGE 
!. STAMP OR ENGRAVE SERIAL NUMBERS OF I RIGS. NASA 0W& NO 000012. ANO PIPS NASA 
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12. ITEM @ TO BE SELECTED 8 MAINTAINED MGONJUCTOfc WITH THIS A9SEMK.V. 

ITEM (j|) TO BE AS &Et m, E D PER NASA DRAWING NO. 1007572 AT 1.5.6. LEVEL. 

SELECT ITEM (35) FROM TABLE I 

a. BOND ITEMS <3§) 8 © TO lTE#T>lTN ITM <3J). 006T MATINS 9URRCES OF ®QD B© 

WITH (35) BEFORE ASSEMBLY 

14. FCR ;^AR£S PROCURED NT ASSEMBLY MUST MEET THE “EMENT OF P*V00020\ 

A TAPE ITEM (g) SHALL K USED AS RGOUMED TO RESTRCT MOVEMENT OF Tl« IMMCSiMTIC CAKf CLiwr 



MARK J2 
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LEVEL ADJUSTMENT. 


WITH NO MSUURKM 


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A/R A/R A/^ vA^KMtBALANCE.OUTER GN*iA__ 
A/R A/R a 75 \A0OfT.BAcAM g.XTEP "(*4BAL_ 
A/R [A/R A/R VS^iGhT, BALANCE OUT£MlQ GRBL. 
A/R [A/R A/P A4CHT. BAJVJCE MlQ GMdAL 


K?2I4QS 
1 000223 
0002 20-6 
000220-8 
I007S SO 
010638 
001477 
1001476 
001 906- k 
00901-031 
1000 076 H 
0014 89 
0014 86 
000270 

|0002t3 

000265 


S/R" A/R A/ft 

t7w A/R U/r" 


V\£K3HT. BALANCE 

MlQ (JMBA 

l 000261 

{5EENJTE6 

36 

BAlAMCF 

S/M 

t00260 

5EEN0TE6 

$5 

/vEiorr.aALAAjCE 

“S/M" 

000259 

fefvME6 

34 

weight. balance 

S/M 

000258 

BEE.idfe 

33 

weight balance 

S/M 

OOu2i4 

5EEN0TF6 

S 

WEGHT. BALANCE 

~s7m 

0 u02« 

ESENOTr 6 

3i 


view E-E 


OUTER AXIS ASS t Y 
" CASE,COVER,"PPER 

" SCREW,But HO SELF LNB S 

“ 5LAre“i|F<5RMATlON- 

" Slate .information 

l LJ 6 P 1 CANT OOW CORNING 


J 

1 

□I 

1 

1 

1 

1 

n 

1 

plate, oentfcaton 

11000021 

24 

4 

4 

4 

4 

4 

4 

4 

4 

4 

SCRE W.a/T HD.SElF-LKiS^ 

X000250-13 

23 

12 

12 

12 

12 

JL. 

12 

12 


12 

SCPE AL ■^AR SOC HD. HEX 

|»00l4e9-« 

22 

24 

12 

12 

24 

72 

TT 

24 


J2_ 

5CPE A/CAP SOC, 1-0,HEX 

10014 99-48 


20 

20 

20 

28 

uL 

2« 

28 

^20 

29 

3CPEW CAP SOC i-OHEX 

1001409-47^ 


2 

2 

2 

2 

2 

2 

2 

2 

2 

FACKING.PPEFOPMEQ *0 RM6 

M000I59-6 

19 

1 

1 

1 

1 

1 

1 

1 

J_ 

_j_ 

RCKNG. =PEFOPF.€D. *0' «N6~ 

1IOOO 59-5 

10 

1 

T“ 

1 

1 

1 

1 

1 

1 

1 

nblve.^resslpe, assy 

1000234 

17 

2 

2 

2 

2 

2 

2 

T" 

~~Z~ 

i; 

(COLPLIva'iALFQUCK.DSCOMvS 

rn 1000135 

M 

4 

4 

4 

4 

4 

4 

4 

A 

4 

[SPRING. FASTENER 

J 100018 7 

• 0 


replaces rev l with changes 


COVER, SPRING rA6TCNEW 
ISCREW, FASTENER 


I PtC tQ NS, PWtroRMID.'D'* RIN 6 
_Z PACKING.PREPOPMEUfO' RING ___ 
a NkCWNfe, PRC FOWMED.-Q-WXG 
I MT.C 08 R ASST BA OUTER A 09 

1 !mt. wO.v, V-Q'Y I x.iTt* AAfo 


I CASE,COVER, FIXED 
I D»SE;COVE^ MOVEABLE 
I OUTER AXIS. ASSEMBLY 
I MACHME ASST CASE CENTER 

•W lOMNCUITUM 


IOOOI65 

»°O Ol66 
001478 
j OOOi>f-l " 
000*59-1 
coo is*-a 
0019 39 . 

Tice 1338 

•000209-OOC 

'i5c 506-1 

000241_ 

000062 
topi sol-Orr 
000069 


J 


1091109110711061 105 1 ,04i j Q3l ! Cgl 


LIST Q> POUTS MO MATERIALS _ 

INERTIAL | **SS5T.r<a* 

MEASURNG UNIT ' * 

assembly . .Ta sra y 

Wu I «... I™.** , C 3i77f 


























~ r • 


4** 


12 


-j 


B 


.1 




n 




IO 


1 SCREW SELECTION CHART | 

DRAWING NUMBER 

USED ON 

100*458-2 

STABLE 

member 

-3 

-4, 

-5-6 

CC 4-59-2 

X!493-i 

MIDOLE 

AND 

OUTER AXIS 

ICO 1499-3 

1001488-2 

ICC,489-4 

*00*438-3 

1001469-5 

*001488-4 

1001489-6 

1001488-5 

011 (021 
C4-! 051 

C7 ' OBi 

ii’ J. 

i Libo 

iooiu 




, Ali‘ 

ksi 

. Hii: 



r ;v 

|<*’ ¥ ■ 



'* 7! 


■t 


RMifr 


G_RO WHEEv. "YPES 

MODULE PART VJMBER 1 

3 SIMCNDS 

1007550 -01 i 

100755 0-051 

2 SIMCNDS 
! GRAPH MC 

1007550-021 

1007550-061 

1 SIMCNDS 

2 3RAPHM0 

1007550-0?' 

1007550-071 

3 GRAPHMO 

1007550-041 

1007550-081 

IMU CQNFIQURAT CN 

-011,-021, 
-031,-04-1 
-051, -csi: 

-071,-081,-091 

HI 


viewE 


typical installation 

SEE NOTE 9 


SEE NOTE S 



NOTFS 

L NTERPRET ORftWNG W ACCORDANCE WITH ML-0-70327 

2. ASSEMBLE $ TEST PER REQUIREMENTS OF ATP lOOOOOlg FTM 1000201 

a SCREW TORQUE REQUIREMENTS ±7% 

A. 10.0 MLB 
a 5.0 N. LB 
C. 1.0 N.LB 
Q85.0 fULB 

E. 70.(7 N. LB 

F. 65.0 IN. LB 

G. 30.0 IN. LB 


H. 3.5 IN. La 


4 MARK CHARACTERS;§|hIGH COLOR BLACK PER NO 1002019 AT- LOCATIONS SHOWN. 
5. ENGRA€ CHARACTERS ]% HGH ANO FILL. COLOR BLACK PER NO 1002019 


f. BALANCE \A€GHTS ANO NUTS TO BE SELECTED FROM APPLICABLE DRAWINGS AND 
INSTALLED PER ATPIOOOOOI. SELECT SCREWS FROM CHART SEE NOTE 9 


?. USE DRAWING NUMBERS I0Q0QI6 OMBAL ASSEMBLY OUTLIVE AND 1000017 
WIRING DIAGRAM FOR REFERENCE 

r . PROTECTIVE COVER.ELECT.NASA DRAWING NO. 1001495, PROTECTIVE COVER .COOLANT. 

NASA DRAWING NO. 100 1494, MOUNTING PAD COVERS, NASA DRAWING NO.’S 1001460,1001464<1001461 

WH^f’^^I^^SSNG^TK^S§l^^u5fIoN^^PROvic^ 0 H?ATER ( p^E < R ,LY 

TO INERTIAL COMPONENTS. USE SELF LOCKING SCREWS, NAS 135C04LL4,0R EQUfV, 

TO SECURE 1001495 TO CONNECTOR MOUNT. ASSY'S (7) ANO r§T) SCREWS NOT TO PROJECT BELOW 

MCwNTTNG SURFACE OH(jT)S (T) REVCVE PROTECT! VECOVER 

MOUNTING SCREWS AND CABLE IMMEDIATELY PRIOR TO INSTALLATION 



-MARK J2 
—: MEW C-C TYP 


-MARK J1 
SEE VCW C-C TYP 


SHOWN WITH NO INSULATION 


9. SECURE BALANCE WEIGHTS.ITEMS (3?)THRU(40) TO GIMBALS WITH SCREWS PER 
SELECTION CHART,a (56) OR® AT REQUIRED LOCATIONS ON MIDDLE AND OUTER 

GIMBALS. SEE VIEW E FOR TYPICAL INSTALLATION DATA. CAUTION: DO NOT INSTALL ITEM (56) OR 
ITEM(?Din LOCATIONS THAT WILL PREVENT FREE ROTATION OF GIMBALS. 

10, TEMPERATURE OF ASSEMBLY- MUST BE MAINTAINED BETWEEN I20°F ANO I40*E 
PULSED INTERGRATING PENDULJM,NASA DRAWING NO. 1000013. MUST BE RECALIBRATED 
IF TEMPERATURE EXCEEDS THESE LIMITS. GYRO PREALIGNED ASSY.,NASA DRAWING NO. 

1000012 MUST BE RECALIBRATED IF TEMPERATURE EXCEEDS 40*F*TO IGOT RANGE 

I. STAMP-OR ENGRAVE SERIAL NUMBERS OF I RIGS, NASA DWG. NO. 1000012, ANO PIPS NASA 
NOIOOOOI3 IN APPROPRIATE BLOCKS PER NO 100209 
*2. ITEM (49) TO BE SELECTED 8 MAINTAINED IN CONJUNCTION WITH THIS ASSEMBLY. 

ITEM (4§) TO BE ASSEMBLED PER NASA DRAWING NO. 1007572 AT I.S.S. LEVEL. 

SELECT ITEM (59) FROM TABLE I 

13. BOND ITEMS (46) S (57) TO ITEI^(T)WITH ITEM (4§). COAT MATING SURFACES OF (46)(47) 8 CD 
WITH (48) BEFORE ASSEMBLY 

14. FOR ~CAR.ES PROCUREMENT .THIS ASSEMBLY MUST MEET THE REQUIREMENT OF PS\OOCZO\ 

15. TAPE ITEM (g SHALL BE USED AS REQUIRED TO RESTRICT MOVEMENT OF THE HARNESS IN THE CABLE CLAMP 


«• COOLANT PASSAGES SHALL MEET THE CLEANLINESS REQUIREMENTS OF ND 002223 
WHEN ITEMS®® 8(25)ARE ASSEMBLED TO CASE,ITEM® 

17. APPLY SEALING COMPOUND PER NASA DRAWING NOt 1006336-000 W SECURE 

- PRECISION resolver adjust pot screw heads subsequent to iss 

LEVEL ADJUSTMENT. 


, 1 ? 



-<a \k 


_ J 0 



& 

|K.T 








5 


:cci;o 











































































2 


* 


.. REPLACES REVISION L WITH I / 

__ CHANGES TDRR '->5C7 _ W' 

N P&MSE.D TCRR iAf33 _ 'I^L^LUM^ 

P REVISED TDRR 14673 isj^ts ] % 

‘ _R_ R EVISED TDRR i5? ,6_ Til 

' S REVISED TDRR 16803 _ n.**# 

T REV ISED TDRR 16807 ,v.«*r AM U 'K 

* U REVISE D TD RR J7o30_1 

" V [REVISED TDRR 2234-4. 
w fiiz/sr o PER TSRR- 23222 Z7 \^r 3 US 
V REVI5EP PER TPRR - 26170 ' l y t * Jlt P J*- 
Z REVISED PER TDRR-2c 71! 9 :** 9 ~3~ -p, 

" TT erriseo pez zi9 4 € £f 

43 I RkViStD ~'v< *1+** y^. 

" AC I REVISED PZR “DRR 35064 3V4R T^t 


, AD ; REVISED r=-3“^RR 33323 



REPLACES REV L WITH CHANGES 



Mnj 

liOiiiaSL__ 

IlSSSnS^SSBl 

1 Inn rinSII BSSSif! 
■iwio—o—■own 


8 , Vjo! i a jC itk Aar? 

CR, FIXED _ 

n?, MOVEABLE _ 
V XIS. ASSE MB LY 
ASST CASE CENTER 


0002 05-000 
0C 5C6-I 
OC024I_" 

iooooaz 
lOcisol-'Ci i 

1000083 


LIST Of PARTS AWO MATERIALS 

INERTIAL 
MEASURING UNIT 


80230 


IOOI5GO 













































































2 


PART NO. NOMENCLATURE. 


QTY 

REQ’D 


1000085 I MACH ASSY CASE CTP 1 

/ 0015 a case com uppep:::: 

100024/ CASE COi/EPF/XEDl^ 
iooozos . i< 5 sa j x _ com Am ; 
1001558 MTWH ASSY /X O-A,. 

/QO/559 MZICom ASSY- /6X O.A. 

1000159-1 ft/CK/Nq P&R/PMED XT P/HE 
/000/59-Z | ---—— 




1000159-3 

iooom-s: 

1000153-6 
IOOOH5ZZ 

ioootn :z:l scpek fastener ii . 
1000/851L. Cdi£RlSPR/H<? FASmtTC 
zooo/87:: spp/A/f, fastener- iin 
tooo/zsn coopl/nehalf, men m 
ioooz34 :: m ve pressure~ assy_ 
ioooozzz plate, /nfopmat/on _ 

1000023~ PLATE, /NFOPMAT/OH ZI 
/00705011 /MU-CTXJ LOAD COMP MOD ASSt 
1001489-JZ SCREW CAP SoC HD HEX 
100/489- 48 | - 

1000250-/3 SCREW BUT WO SELF Lkf 
TOO 1417 /HSOL, CASE HEAT &./*//) 
100/478' /HSU/,CASE HEAT EX (1. H.) 


com ACCESS PsuP. Mod 


PART NO. NOMENCLATURE' 


QTY 

REQ’D 


181 

A/R 
A/Hi 

mi 

A/Pl 

m 

A/P 
Wl 
fl/Pl 
A/P 
A/Pl 
A/P 
A/Pl 
A/P 
A/R 
A/Rl 
A/P 
A/P 
A/P¬ 
A/P 
A/P 
4 ~ 


REVISIONS 


DESCRIPTION 


DATE I ARRROVEO 


RELEASED TDRR. 
TDRR 1077/ 


0 90 5-) 




tJEES&E'lEm 


PART OR 
IDENTIFYING NO. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
* * ± 

00 NOT SCALE THIS DRAWING 


MATERIAL 


LIST OF MATERIALS 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MANNED SPACECRAFT CENTER 


HOUSTON. TEXAS 


6-1-641 


INERTIAL - MEASURING UNIT 


CODE IDENT NO. SIZE 


DRAWING NO. 


APPLICATION 


100150(7 


























































PART NO. NOMENCLATURE" 


QTY 

REQ'D 


1000085 
loo/566 
100014]1 
1000205Z 
1001558 : 
100/559 ... 
1000/59-1 
JOOO/59-Z 
1000/59-3 
1000/59-5 
1000/59-6 
zooo/63 
i000t$2 ZZ 
1000/85 
1000/87 ' 
1000/35 
1000134:: 

/oooozz 

1000013 Z 
/007050zz 
1001489-12 
m1489'48 
100/489-47 
1000250-/3 
100/417 
100/478~ 
/000200> 
1000207 
1000005 
1000074 .... 
1000/03 _ 


MACH ASSY C4S5 CTP 

case cover upper zzz: 
CASE cover Fixed ; 
1QSA 16 X OUTER AX/S 
MT CONN ASSY /X O.A. 
MY COM ASSY !6X O.A. [ 
PACK/Wj P&R/RMED ’O'/p/Mf 


COUEP ACCESS RSVP MOO 


couepzspr/n// fastener: 

2PE/N4 ^FASTENER ZZZZZ 
COOPL/NE HALF, OU/CK P/S 
VALVE PRESSURE „ ASSY 
PLATE, INFORMATION 
PUffE, INFORMATION ... 
/MU-CDU LOAD COMP MOD ASS/ 

screw cap, soc Mo HEX 


SCREW Bum SELF Lkf 
I//SVL, CASE PEA T £4. (PH) 
JNSUL.CASE NEAT EX (L M) 
/ESA /6 X M/DOLE AXIS 
/GSAS /6X INNER AX/S 
STABLE MEMBER ASSY 
HSE ASSY- H/BDLE E/M. 
HSG ASSY OUTER C-IM 




RELEASED TDRR Q <f£, jT7 
TDRR 1077/ 


TDRR 10607 


DATE I APPROVED 


VBSkTEkWKi 

yto riij EEM 

mmm 


PART NO. NOMENCLATURE' 


QTY 

REQ’D 


1000076-1 
1001489-Z 
100/483-3 
100/489-4 
/00/489-5 
100/489-6 
1001488-Z 
100/488-3 
100/488-4 
ZOO1488-5 
100/488-6 
1000270 : 

'100026% Z 

1000263 Z 

/00026 Z 

IOOOZ6I 

/000Z60 

/000259 

1000258 

10002 /4 . 

100O2/3ZZ 

100025Q-JZ 

m-L-4343 


NUT, CLINCH, PLUSH MTO tZ 8 Z 
SCREW, CAP. SOC HP HEX 4 /P 

zizzzzz ■ zzzzzz . a/r 

zzzzzz: Z Z ZZZZ A/P 
ZZZ. _... A/P 

.zzzzz *zzzzz W 

SCREW, CARSOC.HD, SELFLK& A/P 

.zzzzz .....zz m 

ZZZ ZZZZZ" A/P 

zzz:.zzzzzz . a/p 

_zz* _ : A/P 

WE16HT, BALANCE^ 0.5, A/P 
1 " * A/P 

P/P 
A/P 
A/P 
A/P 

A/P 
P/P 
A/P 
A/P 


HE/CUT, BALANCE 


ZZZ MA. 

.ZZ M6Z 

_____ 3/M 

- S/M 

_. S/M 

ZZ ZZSjM 

-_- 1 — s/m 

SCREW BUT HD SELF1X5 
LUBRICANT '. DC 55 ZZZ 



LIST OF MATERIALS 



UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
Yt ± ± 

DO NOT SCALE THIS DRAWING 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


inertial: measuring unit 



DRAWING NO. 


1001500 


INCHES 


■4. I ) : 


^PHOTOGRAPHIC SCALE CHUT , >j 




































































REVISIONS 


PART NO. nomenclature: 


QTY 

REQ’D 


1000085 1 MACH ASSY CASE CTR 
Zoo/566CASE CoUEP UPPEP ZZZ 
IOOOZ4/ CASE COVE# FIXED . 

/000205 IGSA76X 1OUTER AM 
1001559 MT COnNASSY 1 X 0-A. 
1001551 MT COM ASSY /6X O.A. 
1000151-1 PACKING P&RXMED V'R/Mf 
100051-1 Z ZZZZZZZZZ 

I000/59-3 zzzzzz .zzzzzzz 
iQoo/54-5 z 

iooo! 5 i-c> 1 r zzz: zz 

1000163ZZ COVER ACCCSSRSUR Mop 
1000/ n ZZ SO&K FASTENER Z. _ 
1000/85 ZZCQUEPrSPP/A$ FASTENER 
jooo/87 :: fastener z 

I000/S5~z COOPL/HF HALF, OU/CR P/S. 
1000134Zl VALVE PRESSURE . _ASSY. 
tOOOOZZ Z PLATE , INFORMATION 
T000023Z PLATE, /MFOPMAT/ON ^ 
7007050 ZZ /MU-CDU LOAD COMP MOD ASS/ 
100/489-/1 SCREW CAP SoC MO HEX 
100/483 - *9 ~ I 

100/489-47 ^ » : 

1000250-/3 SCREW BUTHD SELF LR<f , 
7007417 ///SUL, CASE HEAT EX. (PM) 

JOO/478 m/JLXASE HEAT EX (IZH.) 
.7000206 t£SA /£ X M/DDLE AM 
7000207 /$SA J6X INNER AX/S 
1000005 STABLE MEMBER ASSY 


1000074 1 HS5 ASSY M/DDLE 5/M. 

1000/03 _ HSO ASSY OUTER G/M 
7000/0/ “ HOOS/H7 0EAP/H5 /XOA 
7000/06 z Hous/A/C pexp/axs 7XMA 
1000015 HO/JS/m BEARING /XIA 
7000075 P/07DPJDRQL/e 


PART NO. NOMENCLATURE 


QTY 

REQ’D 


1000076-1 
1001480-2 
1001483-3 
1001489-4 
J001483-5 
100/489-6 
iO O 1488-zz : 
1001488-3: 
100/488-4 
1001488-5 
100/488 -6 
1000270 
/OOOZ6Z 
100026 3 
100026 Z 
1000261Z 
/000260 
1000251 
J000258 
10002/4 
/0002/3ZZ 
/000250-I 
.M/L-L-4343 


NUT, CLINCH, FLUSH MTD ZZ 8 Z 
SCREW, CAP, SOC HD HEX A/P 

=rz-1 —zz-: />/« 



SCREW, CAR, SoC HD, SELF IMS A/P 

.zzz; : . a/a 

zzzr : z a/p 
zz::: a/p 

_z a/p 

WE/CUT, BALANCE 0.6. A/P 

z__: I zz:zz::: o.&. a/p : 
zzz z~ 054/44. A/p 

:: zz zz..zz m.$. a/R 
.zz zzzz no .: A/p 

___ S/M A/P 

:z - S/M A/P 

ZZ S/M A/P 

.S/M A/P 

:zz__lz:z.:. s/m fi/P 

SCPEW BUT HD SELF LKG 4 ~ 
LUBRICANT DC 55 .. A/R 


RELEASED 77>*R 0 9057 

TDFR 1077/ 


TDRR 10907 _ 

ADPED SHEET Z TD/?R !o9oZ~ 


DATE APPROVED 


mszrzmm 

MEkVlZMWA 

ICTSESRa 



SHT | ISHT Z 


status 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN »f 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
± ±: ± 

DO NOT SCALE THIS DRAWING 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


INERTIAL MEASURING UNITZZ 


DRAWING NO. 



1001500 


SHEET J OF £ 


O I r f I 

| ^ PHOTOGRAPHIC SCALE O NtT j J 
















































































REVISIONS 


QlNOMENCITVTUR 


QTY 

REQD 


jaoDmrz 

/oooo^zz 


/oo/s?o;: 

jms’sf—: 

100/583': 

1000/98'::. 



rooo/sz ~r 
loooofz 
jooodz:: 
/oooi/o: 

10O/49Z-3 
/00/49Z-4 
/oooni : _ 
tooo// f : 

looo/zs\ 

b / OOO/OO- L 

jooo/oo-z 

\ LC00/70-/0 

\ /oooz/9: 

/0070/3. 


SUP R/NC ASS 4o <2»r\ 
B&XVERJRA/USM/TT&t jx 
RESaLv&TRANSM/TTER /X 
7RAtMSM/77K /X 
um/t^Sks/tch . 
BRACRET PETAW/aRt 

contact : z : zz : 
cup Pewa/we- ::: 

8DSP/NS /NSPLA7EJ> Z 
CLAMP TORQUE MOTOR 

<$c//d£ m ps ::: 

so/ps : ia//re 
CU/D£ Hv/PE ...... 

CO/PE IN/R£ 
cu/pe w/pe 

Connectpp zz ;z __ 

copuecTop 

C0NNEC7Z>P __ z _ 

COPP5C70P 

Convector 

Bracket compel tor 

TERM/ML _ _ 

TERMINAL 

Pose _ _... 

Blower 

PECULATOR Z8VDC 


mRT no! 


IOOOZ3Q. 

JOOOZZfZ 

rood/43:: 
/ooois7 Z 
looozic^ 
foo6Z44 :: 
/000097 
/007OZZ 
/000/Z4 Z 
/00OO34 


! NOMENCLATURE ^ Y D 


reactor, saturpqle _ z. 

COVER -CONNECTOR Max/T 2. Z 

Cover comm&tdr raacrlt pz 
Clamp: Slower TZZZZ. 8 ZZ 
CLAMP CAPAC/7D* ZZI 2.1 

cl/p::ootzp„ <?/mbal : ~ t~~ 

z>* ^ —-zzzr“zzzz: z zz 

Ada preamp z 

A//P/NC HARNESS ‘Cf / . . .. 
M//R/NC HARNESS *3/ V Z 



DATE I APPROVED 


ADDED SHEET2 TDRR/090Z- 


lUtA 


rrrmi 



UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
dt ±. ± 

DO NOT SCALE THIS DRAWING 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


INERTIAL MEASURING UNIT. 


DRAWING NO. 

1001500 


2 OF 


•PHOTOGRAPHIC SCALE PHUT 










































































m 


PfcRT NO. NOMENOATURE.: 


QTY 

REQ'D 



1000085 MACH ASSY CASE CTP \ 

too/ see - Case com upper zz 

100014f i: CASE com F/XEO IZ__ 
100020 s iqsa lExzoum am 

100/558 I MT CONN ASSY - /X O.A.. 
100/551 Z MTZCOHN ASSY IPX AA. 

1000159-1 WCKINq P&RXMED VP/Mf 

1600151-1 ~ ~ 1" :z zz' 

looo/59-s ".:z::.:zzrz: z./ 

mom-5 :“zzz zrzzr: :z : / 

/000/51-6 


"iC66m~ SCREW, FASTENER '. ZZZ. 

1000185 z. cover; SPR/Mf fastener : 
iooo/87::: : spehm^fastener : zzz 
1000/251Z. CooPL/NEHA/F, OWCK P/1 
1000134: VALVE PRESSURE _J5SY ^. 
/QQ002&Z :mTEZTNFORMm*czz : 
loooca z. PLATE, INFORMATION Z 
1OO7G50-; m/pmrmDCcMPm/kst 
tOQ 14 83-1% SCREW CAP SOC HEX 

too /483 48 __ „ : 

- 47 . . . .t___: 

100(250-13 SCRBYBCTm SELFLkf 
JQQ141T- t(lSUL, CASE HEAT BLfc/$ 
100/478 /NSUL,CAS£ HEA7EX (l.H.) 

{tp oo 2 oo> : ics a :: /6 x m/due axis 

1000207 K/SAZJ6X INFER AX/S 
1000005 STABLE MEMBER ^SSV' 
1000Q74 -1 Mtj ASSY- MIDDLE C/M 
1POO/03 _ HS6 ASSY OU7ER E/M 

1000 / 0 /:: wusw .feapmjczjxoa 
jooo/oo Housm m/R/M ~/xma 
1000095 Housm Bmp/joc /xjaz: 

1000075 MlPPj72>RQVez::ZZl 

ioooozs.. supR/nc Assy so cm 


PART NO. NOMENCLATURE 


1000076-[ 
1001489 -Z 
100/483-3 : 
100/483-4 
J00/489-5 
100/483-6 
/OO14881Z 
100/488- 3; 
/00 488-4 
/OO1488-5 
100/488-6 
1000270 

/ooou%: 
1000203 
100026Z 
/000201 7 
1000260 ._ 
1000259 Z 
1000258 
10002/4. 
100021311 
/000250-TZ 
MIL-L-4343 


NOT, CLINCH, FLUSH MTO 
SCREW, CAP SOC JM HEX 


screw, cap, Soc no, Sofiko 


WEICHT, BALANCE Z 0.5. 

ZZZZZ ZZZZZZZZO.QZ 

izz z zr: z. . ~ 054 

: zzzz ZZZZZ MR. 
izzzz ::zzzzzzmz 

• S/M 

ZZZZZ ~ZZZ. S/M 
_ZZZZ ZZZZZZ1S/M 

z:zzz _ zzzsj/i 

~~7~ ■ - s/m 

SCREW 8//T HO SELF LKO 

\wmmrzt>c 55 zzz 


QTY 

REQ'D 


Z8Z 

R/R 

A/R \ 

A/R 

R/R 

A/R 

R/RZ 

R/R 

fi/R 

A/R 
A/RZ 
A/R . 
R/RZ 
A/P. 
R/R 
R/RZ 
A/R 
A//CZ 
A/R.. 
R/R 
A/R 
4 





x .JL. 


RELEASED TDRR O <f6 51 

TDRR 10-77/ _ 

TDRR 10907 _ 

ADDED SHEETZ TDRR to90Z- 

TDRR IIQ67_ 


DM CHK OAT* A MM MOV gP 

iJEZ/ y /t\ 

_ AH/ vtL 

_ 7/** JM>UP 

_ dtRjpK 

mT 


0 T> 

C C 
SHT I IshtT 

:m status 



UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
± ± ± 

00 NOT SCALE THIS DRAWING 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMSAIDOC. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 



MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


‘ INERTIAL"MEASURING UNITIZ 


APPLICATION 






DRAWING NO. 

1001500 


SHEET \ OF £ 





















































































-JflZ&SZZ 

J00003ZZ1 


NOMENCD\TUREZ 

SL/fi.B/PO ASS „400»r 




QTY 

RLQD 


PART NO NOMENCLATURE 


70OZB8-. 


IV%W5*M 


mw5zz 
100/5701 
/00/537Z 
100/5831 

moi?di 
/OOO036. 
/OOOO87. 
J000207Z 


100009Z 

jooonzzz 

looomzz 

TOO/49Z-3 
100/4 91-4 
/0O0//71.- 
7000//fH 
7000/2S1 
7000/00-'Ll 

iOOO/OQ-Z 
1000/70-/0 
70001/ 9 “ 
70070/3 r: 


r mj/&rmmM/T 2 i*::zx 

UH/TZSiP/TCP _Zi: 
BRACKET 8ETM/A& - 

courier z : z:zz 
cup /?£ 77 //mvo zz 

80S////05 ' MPL47PX> ~i 
<2/7/^ 

! <&?/£>£Z ZZZIZZ 

5P/OE &//?£ — 

t&'/Ar MOfPZlZ 11111 

&//£>£ H///re a : 1 

copvecm ^.z.. .zz 

covpec 7 z>p-~~:i 1:1 
_C 0 MAj£e 7 t>P .. 

coppoctop z 

Coppeorop zzz 
BfiflCfer <u?pp£c 7 ae : 

teem/pal . . . 

t&m/pal : z zz 

iB/seimiiz. ... 

/Uo/oep imizi 11:111 

/?&QLAT£X 18V0C 


1000/43:11 
/ 000 /S 71 : 
/0QOLS5- 
/000Z44 : 
/000097. 
J007O1Z1 
/000/Z41 

/OOOOZ4 

lOOOZll 


^0/C7d^S4rpP/)QL£^ 
6/PEP _ COPAje&Ol 
com coppz7P4 M4cm^ 
C£///ip :£/4>tuep 1.ZZZ 

CiAMP . CAPAC /7&P. ZZL 

ci/p:ov7zp 5/mbal: 
1 A £>A 11. ..__ZZ 

AdA~ PteAP P z 
W/&P6 ~//AMES *e 1 
Mfi/PC PAPPUS IIS*! 
PLATE tDENT/F/CATK 



LIST OF MATERIALS 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


INERTIAL MEASURING UNI! 



DRAWING NO. 


1001500 


SHEET g OF 








































































































PART NO. NOMENCLATURE.. 


1000085 MACN ASSY CASE CTR 1 

/ 00008Z. case cover movable 
1000141- case cover f/xed - 
iooozos: ig$4 /ex oo7& Am : 
looissd z :: mt conn assy . ix q.a. 

100(559 .: MZ.CONN ASSYIEX O.A. Z 
1000iS9-l PACN/Ntf PRERRMED15R/H6 

iooo/59-z :: .....__izzz: 

IOOOI59-3 :_- zzzzz rizz: 

1000/59-5 j_ 

1000159-t ,., -v . t .— 

IOOI475 1 COVER ACCESS J?SVRpbD 
1O60/EH5Z SCREW! FASTENEPllll 
1000185777 TjO^TSPR/N^ FASTENER 
100018771 5PRjN§JFFST£NER 711777 
10001351: COUPUNE HALF, MCR P/S. 
10001341 VALVE PRESSURE—ASSY- 
10000ZZ 7 PLATE, INFORMATION 1 

1000073 :: plate, information ^ 
100105077IM1PCDU LOAD OOMC MODES! 
>001483-it SCREW CAP SoC WZNEX 

m 148* 48 .. 

1001483-47 HZZ T .J 

100(250-13 SCREW BUT HO SELF Lk<r Z\ 
10014177 IpSVL, CASE PEAT £4. (k. 
1001478 mVL.CASEHEATS* (l.H) 
fOOOZ&o ' tOS A 77.18 X MIDDLE AXIS 
JOOOZOT 1$SA 716X INNER AX/S 

JOOOOOS STABLE MEMBER ASSY 


QTY 

REQT) 



1000074 

1000/03 


HS$ ASSY-MIDDLE 5/M. 
HSO ASSY OUTER 6/M 


part no. nomenclature;:; 


NUT,CLJNCh, FU/SH MTO 
SCREW, CAP, SoC HD HEX 


QTY 

RLQ'D 



SCREW, CAR SOC HD, S&FLR& | A/P 

A/R 
A/Pi 
A/P . 
A/ff! 
A/R: 

\m~ 

i~064me. I A/R- 
~ hi mi a/r 


WEIGHT, BALANCE 






UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN »f 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 




REVISIONS 

DESCRIPTION 

' RELEASED TT>RR Q q(, SI 

' TDRR IQ-771 _ 

' TDRR 10907 _, 

ADPED SHEET 2 TDRR lO<fo2, 

TDRR H067 _ 

' TDRR 1133+ _ 


DR CHK DAT* APPROVED 

_ hP \ 

_ hj<*6 jJad vV 

_ 7JU44 ZSlJP 

_ /fJmif O M/lbN 

ijJ«jr\jAUA Ml) 

- 


£ £ 

D 2> 

C C_ 

SMT I iSHTF 

:rev status 


REQDI IDENTIFYING NO. I OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 



MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


ihertial: measuring unit' 


DRAWING NO. 


1001500 




















































































vrm i 
e£D 
SGSfffii 




r/#;#.#vgy 


W/Mmi*!**** 








I6oono-/o Fuse 
/oooz/9: 6£ove% 

/0070/3. F&OLATC* 28Vt>C 





UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN »f 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
st ± ± 

DO NOT SCALE THIS DRAWING 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


APPLICATION 




MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


INERTIAL MEASURING UNIT 


S89SSE®| 



CODE IDENT NO. I SIZE 


DRAWING NO. 

1001500 


SHEET g OF 





















































































PtkRT NO. NOMENCLATURE." 


MACH ASSYCASE CTR 





/ 00014f 
lOOOZOSI 
1001558 Z 
1001559 ... 
1000159-1 
1000159-1 
1000159-3 
1000159-5 
1006159-6 
100M15 I 
JOQOiJZIZ. 
1000185 z 
/0OO187 : 


1660134Z 
10660ZZZ 
1000013 ~ 
1001650Z 
1601489-19 


(601483- 



'000150-13 

10Q1477 

1001478' 

(000206 

rooozor 

1000005 
1000074 
foootOZ .... 


SCREW BCTHOSELFMcQ 
(((SOL, CASE HEAT 
mOL.CHS5 MAT0T(l M) 
10 SA J6 X M/DOLE AXIS 
IQS A 16 X INNER axis 
STABLE MEMBER ASSY 
HSQ ASSY...M/OOLE Q/M 
HSG ASSY 007ER 6/M 


PART NO. NOMENCLATURE 


1000076-1 

100148$-Z 

1661489-3 

1001489-4 

1001483-5 

100/439-6 

1001488-1 

100/48853 ’ 

1001488-4. 

1001488-5 

1001488-6 

1000270. 

' IOOOZOZ 
10002035 
100026ZZ 
100026! 7 
tOOOZGO _ 
1000259 
1000258 
1000214 . 
1600213. I 
1000250-1 
m-L-4343 


NOICUNCH. FLUSH MTO 
SCREW, CAP.SOC HO HEX 


SCREW,CARSOC HO, SSLFLKO 


WE1CHT, BALANCE I 0.0, 

- 1 -:: mi 

__ .-Q&jfMQ. 

-:zzz ZZZZZ MA. 

- --- - mg: 

. S/M 

ZZIZ ZZZZZ S/M 

-zzzzzs/n. 

IZZZ - S/M 

; . * iz zi : s/m 

SCREW 80THO SELF 1X0 
U/BtlCANTZ DC 55 


QTY 

REQ’D 

: 8 
.A/R . 

a/r. : 

A/R 

A/R 

A/R 

A/HI 

A/RZ 

A/Rl 

A/R. 

A/R. 

A/Rl 

A/HI 

/f/Rl 

A/R 

A/Rl 

A/R . 

m 

AA f- 

A/R 

A/R 

4 ~ 



REVISIONS 

DESCRIPTION__ 

' RELEASED TDRR Q 90 51 

' TDRR 10-771 _ 

' TDRR 10907 __ 

ADDED SHEET Z TDRR Io9o2~ 

' TDRR 11067 _ 

' TDRR US3+ _ 

'TDRRII89S;__ 


DM CHK DATE APPROVED 

Tung hr\ 

_ hjvHi jKHL uH 

_ 74*0 

_ ffJttif &+ Jf t 

zjjvUt jAu/SjE 

_ 28 Jvctf Auf 

_ l9Ao*lt l *jA M. 


SHTI ISHT2 

;re\/STATUS 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
± ± ± 

DO NOT SCALE THIS DRAWING 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 



mmmsE, 


APPLICATION 



mm 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


inertial: measuring unit: 


DRAWING NO. 

1001500 “ 













































































REVISIONS 




AMO TNI FACT THAT TMK DOVCRHMKHT MAT NAVI FORMULATED. FURNISHED. OR 
IN ANT WAT SHPPLIKD THE SAID ORAWINOS. SFCCIFtCATIOMS OR OTHER DATA IS 

1 NOT TO DC REOARDCD OT INPLICATtOH OR OTHERWISE AS IN AMT MAMNES 
LICENSIMO THE HOLDER OR AMT OTHER PERSON OR CORPORATION, OR CONVEY* 
IR E AMT RISHTS OR PERMISSION TO MANUFACTURE. USE. OR RILL AMT 
PATENTED INVENTION THAT MAT IM AMT WAY RE RELATED THERETO. 


N0MENCLATUR1 


QTY 

REQD 


PART NO NOMENCLATURE 


QTY 

REQD 


IOOOLQ8 fenCTdt S*rvfi/)QL£ 

joooiz f gw &p <sj wAj&Tae moat 

toooi4z ~ C 01 /& Cto/uzm? fifijcm 

/OOOIS7 Cottip 3u>(4j£f 
/eool 3r, ClAMP CAAK/7PR 1 
/ooozH ci/fi ovrefi 0 /mbal 
1000017 At>A 7 TZTZZY 

/C07OZZ APA Pfc/IMP _ 

i000tl4 Z H//&A/E M/M£SS '<S ' 
1000014 Mfi/HC Mfiju&s *6*; 
100002 !" PLATE 1DEMT7FICA770 


\ -n -1 --- 

J SYM ZONE _ DESC OPTION _ 

J ~g ADP£D SMEE T2 TQRR/Q9QZ. 

Q D_ _ TDRR H067 .... 

® _£ _ TOR*. 1133+ _ 

F TDRR. U8«3S- 


DR I CHK DATE APPROVED 


' ZtJriiV 4*4 (Jjjj 




IOOI 506- 2 I NTER6/MBAL SO^SSY CA Z1..7 
1001508-2 INTERSIM94L 5UfM5SY /X M<4 j 
10015 10 - 2 INT£R<SW8AL SU0-/W5Y >X IA t 

IOOI5Z6 CASE Covet, UPPER / 


iooot7o-/o Fuse .7.. .. 

/oooz/7 :z 6/oveR 

/0070/3 : F&OLATOC Z8VPC 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES INSTF 

CAPACITOR VALUES ARE IN »f < 

RESISTOR VALUES ARE IN OHMS —— 

TOLERANCES ON DRAWN . 

FRACTIONS DECIMALS ANGLES CHECKED 

DO NOT SCALE THIS DRAWING APPROVE[ 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


INERTIAL MEASURING UNIT 


APPLICATION 


APPROVED | 
MIT _ 


APPROVED 

MSC 




CODE IDENT NO. SIZE 


DRAWING NO. 

1001500 


| SHEET £ OF 



INCHES 


*9mm«C'M*eg4M3r i 


































PNRJ no. NOMBslQATURe:: 


1000085 [MACH ASSY CASE CTR 


QTY 

REQ'D 



100/558 l 
100/559.. 
1000/59-/ 
1000/59-1 
1000/59-3 
1000/59-5 
1000/59-6 
{00/475 ~ 
iooo/w :z. 
1000/85::: 
/000/87: 
/ooo/zs~: 
/oooism : 
/oooom :r 

/QOOOZ3 z 
(007050 ; 
100/489-it 
1001489-48 
100/489-47 
1000250-/3 
100/417 
JOO/478 


CASE COVER F/XED ~~ 


MTConN assyjx oa. 
MTZCONNASSYJ6X OA. 
ft/CK/N^ PfE&RMED ’O'/p/Mf 


Cove# AccessJsvfi m 
5CREK FASTENER Z ZZ 
COVER, SRR/N/f FASTENER 
SFEJN9^FAS7ENER~ZZ^ 
com/AifT/Ai^mc/t p/s. 
VALVE PKESSUffi JISSY. 
PLATE:/NFORMAT/o F 
FLUTE, INFORMATION 
/HU-CDU LOAD COUP MOO AS/ 
SCREW CAP, SoC HP HEX ; 


SCREW BUT HD SELF LF<f 
//(SOL, CASE HEAT &. (RWj 

in sue, case heats* (i. m)\ / 




PART NO. NOMENCLATURE “ - 


1000076-V NUT, PUNCH. FLUSH MTD 
/00/489-Z SCREW, CAPJOC NO HEX 

/00/483-3 ;zz . . 

100/489 - 4 ^- 

100/489-5 :ZZZ~ ... ~. 

10QJ4S 9-6 i - ZZZZ 

1001488- Z SCREW, CAP.SoCHD, SELFLN& 
100/48 8 -3 ..ZZZZZ1. 

100/488-4 -"-- 

too1488-s z:.: ;: zzz~zzz: 

100/488-6 _ ~ ’' ZL.. Z . 

1000270 Z WE/CUT, BALANCE Z OO. 
/OOOZS ? 0.0. 

looozc 3 z zzzzi z“ 055/14 

1000261 - -- - ““ z no. 

iooozci : ~ /f/r~ 

/000Z6O __ S/ M 

IOOOZ59 ZZTZ S/M 

1000258 : _ S/M 

1000 Z /4 ZZZ S/ M 

(0002/3 Z r~ * 3/fj 

/000250-1 : s&fer /w> self lro 

mil-l -4343 lumcm: ocss: 


QTY 

REQ’D 



REVISIONS 

DESCRIPTION 

"RELEASED TDRR oqosi 

TDRR 1077/ _ 

TDRR 10607 __ 

APPED SHEETz TDRR 0902- 

TDRR 11067 _ 

TORN H&9+ _ ' 

TDRR. IISES' _ 

TDRR IZST4-—---- 


OR CHK DATE APPROVED 

vm 1 

_ vX 

_ 740* j&R UP 

_ /fJm/A a*&\ yL 

_ 2HyUf\jQU/\ lA 

_ Z8j«.Cf JtHf fyJ 

_ !9Ai*t4*J/i I (illL 


SHT I [SHT2 

■REV STATUS 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN »f 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 
± ± ± 

DO NOT SCALE THIS DRAWING 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


INERTIAL^MEASURING UNIT! 


DRAWING NO. 


APPLICATION 

























































































































































































ORL [RATIO N WNATttOTKR; 
TNK COVMNNtMT MAT HAVK FORMULATED. PURNISMKO. OR 
AY KMPPLItD TNK SAID ORAWINM. SPECIFICATIONS OR OTMKR 
MOT TO BC RRRARORR RT INFLICP 


UCHWH TNK NOLMCR OR ANT OTNKR PERSON OR CORPORATION, OR COMYKT- 
IR Q ART RMNTS OR KRNIBBtON TO MANUFACTURE. UM. OR SRLL AWT 

PATVMTtS irvkntkm tmat ray in ant vat bk relates thereto. 


PART NOT nomenclature: 



QTY 

REQ'D 


PART NO. NOMENCLATURE 


. QTY 
REQ'D 


MACH ASSY CASE CTP 





1001558 z 

10015591 

1000159-1 

1000159-1 

1000159-3 

1000159-5 

1000155-6 

1001175 

1000/99 T. 

1000185 

10001871 

ICooiZSH 


case cove/? fixed 


MT CONN ASSY. 1X O.A. 1 
MT COM ASSY 16X O.A. .. / 
PACKING PEE FORMED V'R/Mf Z 

I .* 


toooozzi 

rooooan 

10070501. 

1001'189-/t 

1601489'98 

1001489-47 

100C250-13 

JOQ1417 

1001478 


COVER ACCESSJtSVP MOD 
SCREW", FASTENER 

meRiSPR/*<r fastener/: 

SPRING. FASTENER 11//./ 
COOPLtNE HALF, <$V/CK P/l 
VALVE PRESSURE ASSY. 
plate 1 information ii 
PLATE .INFORMATION ^ 
1MU-CDU LOAD COMP MODES! 
SCREW CAP. SOC MO NEX 


SCREWBVTHDSELF U<r 
IflSOL, CASE MEAT £X. 0?H) 
mDLXPSE MEAT EX (l. M) 


1000076-! 
1001489-2 
1001489- 3 ; 
1001489-4 
1001489-5 
1001489-6 
1001488-Z 
100/488-3 
1001488-4 
1001488-5 
100/488 -6 
1000270 
IOOOZ69 
1000263 
100026Z 
1000261 ~ 

1000260 _ 

1000259 
1000258 
1000214 ! 

10002/3 Z 
1000250-1. 
MIL-L-4343 


NUT, CUNCR, FLUSH MTD I 8 Z 
SCREW, CAP, SOC HD HEX/ 8/P 

I */* 


REVISIONS 

DESCRIPTION 

' RELEASED TV HR. Q q(, f-} 

: TDRR 10-77 / _ 

' tdhr toecrr _ 

, iPPED SHEETZ TDRR lo902- 

' TDRR IIQ67 _ 

' TDRR HQ34- _ 

tprr iievs - _ 

: TDRR 12rt4- ~ _ 

■ JDRR_ &IOQ _ 


NU _ 

hJv'b /NHL 

4*\ yL 

' Htut xJ J 

!9Ao*t> ’aj/g 
~ 53ep64 lid# Wtv 

ZA&rMX&tl wit. 



SCREW, CAP, SoC HO, SELFL/& A/fi 

~ .~ 1 zzzzznz: p/p 

zr z zz z : 'zzz:zz - ' fi/P : 
zrzzzz a/p 

._:_z\* 8 /R - 

WEIGHT, BALANCE : 05. A/P 

0 .0 : A/P 

zzz: zzzz 054m .6 a/P 

zzz : zzzzz : no. a/p 


S/Ft A/p. 
ZZZ ..... 1.1. S/M A/P 

: S/M A/P 
SCREW BUT HD SELF LKO 4 
W8HICANT DC 55 . A/P 


’ '/f#AIS’F«NN 4 


PART OR 
IDENTIFYING NO. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


INERTIAIZ MEASURING UNIT 


























































































































































*m USCB TO* ANY run rose OTHER THAN IN CONNECTION WITH A DEFINITELY 

RELATED ROVERNNENT PROCUREMENT OPERATION. THE UNITED STATES •OVERH^ 

?S T «I5%S£ r CLJ® WW>"««tlTY NOR ANY ORL.RAT.OM WMA^oUlfc 
" AT H * vf PORN Ul. AT ED, FURNISH OR 

J**’ 1 *’ * AI ° MAW,N **. SPECIFICATIONS OR OTHER DATA IS 

?*_ V. •■"■•CATION OR OTHERWISE AS IN ANY MANNER 

UCENSINR THE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY* 
INO ANY RISHTS OR PERMISSION TO MANUFACTURE, IIMLOR SELL AJIT 
PATENTER IMVEMTIOM THAT MAY IN ANT WAY SC MOATBR TNKMTOw 


NUTT 


PARTS LISTED IN THESE TWO 
COLUMNS ARE COMMON TO ON, 021, < 


PART NO. 


1000085 

/00024/Z 

4000105 


(00/558 Z 
100(559 1 
(000 (59- / 
1000(59-1 
(000159-3 
1000(58-5 
(000(58-6 

(00(475 ~ 

* 

(000(99 T 
(000(85 7 


(000(3551 

(ooozm 

(0000ZZ 
(000023 7Z 
(0015 50 - 
(001489-tt 
(00/489- 48 
\(00(489’47. 
(00(250-/3 
\IOO(417 
(00(478 

T00O206 = 


i000207 


1000005 


1000074 

( 0 00(03 




-(000/06 


1 00009S 


10^0015 - 




NOMENCLATURE “ 


MACK ASSY CASE CTR 

MMArue- 


CASE COVER FlXEDTI^ 
^0 S A (6 -X fitWT 4.*/g 


MT CONK ASSYZ (X 0-A 
MFCONN ASSY^(6X O.A. 
PACKIWj PEEFORMEDWMC 


COVER ACCESSj/SV* MOD 
SCREW, FASTENER 
COVEPTSPP/NLf FASTENER 
SPiJAJ^ FASTENER Z7Z77Z 


C 00 PL/M 6 HALF, OV/CR P/S. 
\VALVE PRESSURE ASSY. 
PLATE, INFORMATION J 
PL/fTE, (NFORMAT/ON 
(ME-COU LOAD CtiMPMOD ASS^ 
I SCREW CAP, SOC HO HEX 


i 


SCREW BET MB SELF LR<f 
fSNL, CASE MEAT 6t.(Pty 
mUEXKSE MEAT EX (l. M) 
Hr-SA . MS X' MW>U E POS- 


t$SA (&*-■(NN£* A*($ 


STAPH M£*/&gR ASST 


-MS$ ASSY tt/em 


4 4SG- ASST OUTER \S(NF 


Miu ' S/,"/?, 5rn;?atts \nos . 


03/ CONHIS U RATION 

rvr-Y / \ I 


QTY 

REQ'D 


/ 

/ 

Z 

z 


I. 

z 

/ 

4 ‘ 

4 

4 


2 

f 


/. 

r 

(Z 


30 

: a 

/ 

( 


.(BS9PLMC MM* 


t teiJSWS P&tpttfT-rr j$r 




'ktPPttC Assy sngtivr 


=fc 

=£*" 




/; . .\ 


\ 


PART NO. 


(000076-[ 
100(489-Z 
1(00)489-3 
(001489-4 
(00(489-5 
[100(489-6 
(001488- Z 
(00(488-3 
(00(488-4 
(00(488-5 
(00)488-6 
(000270 
(OOOZ69 
(000263 : 
(00026Z 
(00026/ 7 
/ 000260 _ 


(000259 ~ 
(000258 
(0002 (4 2 
\ (0002(3 7. 
(000250-L 
MIL-L-(343 
10000 z 1 

\l000205 
lOOOZZO-S 

M002U-6 


loooizr 


nomenclature: 


NUT, CLINCH, FLESM MTD 
SCREW, CAP, SOC MO HEX . 


SCRE W, CAP, SoC ML>, SELFLMS 


ME (CUT, BALANCE 0.6-. 

: . . 0/k 

ZZZZI.73&4M& 
777777 (45 
7777777M.57 

_ S/M 

—7777 8/M 
.. 77 . 1 ,. S/M. 
7. 77 S/M 


7Z7777777S/M 

SCPEW BET HO SELF IRO 
LUBRICANT 7 DC 55 ~Z . 7 
PLATE IDENTIFICATION 

1GSA 16 OA r::: 

C LA/A PC ABLE Z IZZZZ . 
CLAMP CA BLE;T"". 


WAS HE C ABLE CLAM 3 















— 

NEXT ASSY 

USED ON 

| APPLICATION 


QTY 

REQ'D 


78 1 

A/R 

A/P 

A/P 

8 /P 

m 

A/P 

m 

F/p 

8 /P 

p/p 

P/p 

A/P 

A/P 

A/P 

A/P 

A/P 

A/P 

A/P 

A/P 

A/P 

4 

A/R 


f 


l 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLE! 
± ± ± 

DO NOT SCALE THIS DRAWING 


MATERIAL 


3 


REVISIONS 


Q 

Q)_ 


B 9 

J 233 

DESCRIPTION 

m 

[QQ 

DATE 

APPROVED j 

m 

mi 

RELEASED TDRR 0 90 51 

m 

HI 


wmwm 

ES 


TDRR (077/ 


HHI 1 


jfytWM 






7 Jul ^4 

i 

1 





WfMfi 

Eraiffii 

13 







WM 

a 


TDRR H 99 + 



28j«.a 



B 


TDRR. liens’ 



iffPfi 

wn 

mi 



TDRR— 12 ^ 4 - . 



\& 5 ep& 

MM 

;E 13 

□ 

— 

TD R R_ / 31 OO _.. . 

j 

s 



WM 

u 





TZSSM 

EZ 2 

iW 


7v'/*V *Mo 




rnnum 


WMVteu 


immcr- 



U F PE7R- 


KZKSE7KC7F. 




nvumr. 




JoWom 


mm 


M IS A1S5CZ 
'j-ASSX- 


mmk axis Ag.gj 


WMVVJsaiaw&m 






■="t 


oEmm 


ar y, m o q 


QTY 

PART OR 

MATERIAL 

NOMENCLATURE OR 

FIND 

REQD 

IDENTIFYING NO. 

OR NOTES 

DESCRIPTION 

NO. 


LIST OF MATERIALS 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 



MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


DRAWN R <S S 


INERTIAL MEASURING UNIT - 

. r ■ - 


CODE IDENT NO. 


SCALE 


SIZE 


DRAWING NO. 

1001500 


| SHEET 1 OF 2. 


1 


























































i 


NOTICK - WMCN ROVERNMKNT MAWINW. SPCCIFtCATIONS. OK OTMKR DATA 

ARP UUD FOR ANY FUNFOSC OTHER THAN IN CONNECTION WITH A DEFINITELY 

RELATED •OVERNNENT PROCUREMENT OPERATION. THE UNITED STATES SOVERN- 

NENT THEREBY INCURS NO RESPONSIDILITY NOR ANY ODLI4ATION WHATSOEVER: 

AND TNE PACT THAT THE SOVERNMENT MAY HAVE FORMULATED. FURNISHED. OR 

IN ANY WAY SUPPLIED TME SAID DRAWINGS. SPECIFICATIONS OR OTHER DATA IS 

NOT TO BE REGARDED BY IMPLICATION OR OTHERWISE AS IN ANY MANNER 

UCENSINR TNE HOLDER OR ANY OTHER PERSON OR CORPORATION. OR CONVEY. 

IN4 ANY RtRHTt OR PERMISSION TO MANUFACTURE. USE. OR SELL ANT 

PATENTED INVENTION THAT NAY IN ANY WAY BE RELATED THERETO. 


PART NO. 


10QOQ& = 






toaoott 


/oo/srfo 




toot~5&3 




y?&xm 




)'\9&9®0p' 


MX12&2- 


toootsr- 


jQ&ilS Z. 


tC i QGOVZ 


jocimtZ- 


tasatfc. 








tOOUM f 


NOMENCLATURE!, reqd 


Sh>P ft/K? * fc' tiO F 




kt 


te r 5m f sr Tftimmm , 


jLiUtT-. 


&Mto£T..4 > £T4WtM / 'r~ 


•lVUT#C 


t n H> g* ■ 








tSiltPS ■ tA/tR Sz 


ift/ltif. M££i 




Ctnpf W4 gPe= 




timKnai7i^ 




faixvzs 


■fWOJW-T 




/&W/70-/& 




/Q07Q/& 


r }VJA)V££ 7t> * -_ 




7&wajal- 


■Fm& 


tinitupg- . 


/Pfiiuttirtvr ssjrpt^ 


*• * • 

• • •• 


=5* 




-+8 


3? 


PART NO 

NOMENCLATURE 

QTY 

REQD 


ft&CW? -g#7UJ?j3&LE ^— 

-- ' 




WQ&t* 3--— 



Wuut^f - 


•9 — 



.<Ly 

fOOQ? TT—- 

. A to A ■ ■■■—■--—- 

-9- 





r4^i¥/w ■■ " 


inOOfLH 

/oocozi 

/ /\XS * - f 



PLATE /DEA/VF/CAm 

tA4wr&~ rvt*-Anr y*/y 

/ 

t \jt tt ns-ti&z* 

Iff tfJQrrt a^= 

f 

tAA / ■P'/A— -4—-i 

W TT&K /A 4mA A g/A9-4CC»* / & j 



'W-imrEiffrjGmL I i A 

—f— 



— 1 ■n.. 


1 LlN*lTg»<lfcS»iM—Clin. A —IV T A- 

; •:: . 

IOOl5&6> 
1001501 

10002051 

100,50G-Z 

CASf l/PPER 

AXIS ASSY 
7<f54 /&X007ERaxis 
K jSA /X007ZJ? AXIS 

/ 

/ 

/ 

f 

^ ->- 


. 



REVISIONS 


SYM ZONE 


ADMO SHEET2 TQRR/090Z, \ 


DESCRIPTION 


TPRR H067 


TDRR lies* 


TPRR. IISES' 
TP RR llfltf- 


TPRR 13100 
7~///S S#£ET Dii£t£D 

TDRR 73370 _ : 


\2U«4 




WA 




\2iJtun 


ieA*of\ 


\85tPG4 


(?4SOTC4U04| 




APPROVEO 


fJr 


&4 


J0m 


~W 

3 


m 




5 








* 










NEXT ASSY 

USED ON 

| APPLICATION 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN »f 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

± ±i ± 

DO NOT SCALE THIS DRAWING 


MATERIAL 


QTY 1 PART OR MATERIAL NOMENCLATURE OR FIND 

reqd| identifying no. or notes description no. 

LIST OF MATERIALS 

MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 

MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 

OP AWN 


INERTIAL MEASURING UNIT ' 

rHFr.KFn 


APPROVFn _ 

!3Ui^ 

APPPOVFn t f 

U 



APPROVED 

m i t frl// 


CODE IDENT NO. 

SIZE DRAWING NO. 

C T 1001500 _ 

APPPni/FfyO CJ ScT “Ty 

n 

MSC 

DATE 

SCALE 

(SHEET g OF 2 


INCHES 

■ J. * 1 i 

O I T 

photographic scale oner 


j 


































mMsmm 

PATtNTCD INVENTION THAT NAT IN ANY WAT M EELATEB THEACTO^ 


PART NO. NOMENCLATURE. 




1000085 

100014 / 

/cwzo5 = 


MACH ASSY CASE. CTR 

MO t M/Vr£= 


parts listsd imthsse two 

COLUMNS ARE COMMON TO 0/1\ 02l,< 

03/ comsunmm. 

QTY 
REQ'Dl 


| CASE COVER FIXED 
I$SA 16 X i ^ ‘ n T 1 4Wt- 


1001558 
1001551 
1000151- / 
1000151-1 
1000151-3 
1000/51 -5 
1060151-6 
1001475 
iOOOiSS 
1000185 
1000/87 
1000/3S~ 
1000194 
10000Z1 
1000023 - 
1007550 
1001489-1* 
/00/489- 48 
100/489-47 

1000250-13 

1001477 
1001478 


\/iT~CONNASSY-.JX-&A.. 
MT CONN ASSY- I6X O.A. 
PACKING PREFORMED "O'R/W- 


cover Access Jsvfi m 

SCREW, FASTENER 

cover; SRR/N/f fastener 

SPR/AA}, FASTENER I- 
COOPL/NS HALF, QUICK P/S. 
VALVE PRESSURE ASSY. 
PLATE a INFORMATION 
PLATE, INFORMATION 
\lMU-CDO LOAD COMP MOD 
SCREW CAP Ttf* HP HR* 


SCREW BUT HD SELF LN<r 
1(1 SUL, CASE HEAT EX. (Rh\ 
IN SOL, CASE HEAT EX (L H) 



PART NO. 


nomenclature 


QTY 
I REQ’Dl 


1000076-1 
100148$ -Z 
100)488-3 
100)489 ~ 4 
1001483-5 
100)489-6 
1001488- Z 
100/488 - 3 
100)488-4 
1001488-5 
1001488 -6 
1000270 
100026 ? 
100026 3 
1000261 
100026/ 
1000260 
1000251 
1000258 
IOOOZI4 
/OOOZ13 
(000250-1 
MIL-LM 343 
10000 2 1 
1000205 
IOOOZZO-S 
1000210-6 

1000111 
1010838 


NUT, CLINCH, FLUSH MTD 8 

SCREW CAP.SOC HD HEX R/R 

A/R 

m 

A/R 
A/R 

SCREW, CAP, soc HO, SELFLF& I R/R 

1 m 


WE1CHT, BALANCE 


SCREW BUT HD SELF l <6 
LUBRICANT DC 55 
|pt ATE IDE NTIFIEAT1 ON 

GSA U OA 
CLAMP CABLE L"TT.. 
CLAMP CA BLE 

WASHED CABLE CLAM 
ADHESIVE 














NEXT ASSY 

- *_ 

USED ON 


APPLICATION 


4 

__ A/R 

UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

dt * 

DO NOT SCALE THIS DRAWING 


MATERIAL 




ZONE 

REVISIONS 

DESCRIPTION 

DR 

Pf6 

CHK 

51 

DATE 
—i -; 

APPR< 

5VED fl 

<ar 

TT 


RELEASED TDRR 0 16 51 




yd 

—rrw 

TTaI 


fr>RR m~77/ 




WML 

m 


_ 

' 

7Jut 44 
NJutlf 

WW 

43+ 

Ki 


3 


TDRR 10907 

V 

Q 


ADDED SHEETZ TDRR. !OHOZ~ 


_ 

) 

ff 

Q 

IT 


-rn/PP H0A7 



ZkJuUI 






28Jutti\ 

-H 

My 

>r| 

f 


TDRR ))334- 



tdpR. II8QS” 




^4 



— 



M+ 


•7=T~ 

--1 

TDRR—T25T4- 

M 

H 

—- 

TDRR - 13\00 -‘ : 

_ 


24SEPK4 

A&M- 


& 

T~ 


SHE El 2 DELt'tll 
rnkS 13516 



I20CT 


11 


/tV/WW 


Lnwm 

5iT 


TDRR 


- - 

AtWA 


ll&SR 

C 


REPLACED BY REV M W T H 
CHANGES TDRR 14307 

- -■■■ 

. 

ji7 ms 

4B# 

\m 


I 0015 OLi', 

worsv&j 


001505. 


CSSA” JX OA 

I (7 S7T~IY ~ Q A. 


Z&SEL C OV ESZUmES; 


COVERZMOV 




tmeiBammm 


mm 




jnST JTA ^TSSSX 


mTrnmmAWttkTm*: 


XI 


EH 


OTJL 


B£M 


REPLACED BY. REV M WITH CHANGES 


QTY 

REQD 


PART OR 
IDENTIFYING NO. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


DRAWN . 
CHECKED 
APPROVED 
APPROVED 


6-1-141 




E-l-U 


LI ST OF MATERIALS 

MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS _ 

MLRTI AC MEASURING UNIT 


approved 
MIT 


APPROVEI 
MSC 




code ident no 


DATE 


SCALE 


DRAWING NO. 

1001500 - 

[SHEET \ OF I 


3 




























m 1 *«.T" 

ACVISIOMS 

OMCMmON 

1 wi IUZSST 

! v, i REPLACES 
| 1 CHANGES 

REViSiON - WITH 
TDRR -*3C 7 

tj0.rli.V1 


SEE NOTE 38 



S3 


fH- 


fH- 




’ F-F 


E\*~ 


Eh- 



E-E 


REPLACES REV L WITH CHANGES 




m 




UMUM OTKWWM «KC*MO 



TnTtMSTi rST "* 



pmctnm mm •*“ 





DO mr DB8U 1MD OMMW 

1C 15000 

ouoonoo 

WMML 

nut mm 

UtCO ON 1 


1 - 



1 


4 

4 | 

4 

WASHER.CABLE CLAMP 

000223 



52 

1 

1 

1 

CLAMP. CABLE 

000220-6 



51 

3 

3 

3 

CLAMP. CABLE 

000220-5 



50 

1 

1 

1 l 

MU-CDU LOAD COMP MOD 

007550 


EE NOTE 12 

49 

a/r 

VR / 

UR 

ADHESIVE 

010838 



48 



1 

NSULATION CASE HXCHR RH 1001477 1 



47 

----- 

T~ 

1 

NSULA T ION CASE HXCHR LH 

001475 



46 

1 

“ 


NTERGIMBAL SUB-ASSY IX OA 

001506-2 



45 

1 

“Z - 

"TZ" 

OUTER AXIS ASS'Y 

001501-031 



44 



1“ 

JJT. CLWCH.FLU5HHVt)UNlfcU 

000076H 


SEE N0TE6 

43. 

A/R AAJ 


SCREW. CAR SOC HO. HEX 



SEE NOTE 6 

42 

A/R 

VR 


SCREW.CAPSLF-LKG SOC 1-0 



SEEN0TE6 

41 



-fa 

/WEIGHT RAI ANCE OUTER GMBAL 

000270 


5EENOTE6 

40 

A/R ^ 

A/R 

A/P 

/WEIGHT. BALANCE.OUTER GMBAL 

000268 


SEE NOTE <5" 

39 

A/R 

A/R 

A/R 

l 

l 

§ 

<n 

000263 


5EENOTE6 

38 

A/R 

A/R 

A/R 

WEIGHT. BA-AMCE MlQ GMBAL 

000262 


5EENOIE6 

37 

A/R 

A/R 

A /Q 

WEIGHT. BALANCE MlQ GMBAL 

000261 


5EENCJTE6 

36 

A/R 

A/R 

A/R 

WEIGHT. BALANCE S/M 

1000260 


SEE NOTE 6 

35 

A/R 

A/R 

A/^ 

WEIGHT, balance S/m 

000259 


SEE NOTE 6 

34 

A/R 

A/R 

a/r 

WEIGHT, balance S/m 

000258 


SEE NOTES 

33 

A/R 

A/R 

av^5 

weight, balance S/M 

000214 


5EEN0TF6 

32 

a/r 

A/R 


WEIGHT BALANCE S/M 

IGG02I3 


SEE IMOTr 6 

31 


1 

_ 

OUTER AXIS ASS'Y 

1001501-021 



30 

1 


- If-ASE. COVER.UPPER 

1001568 



29 

4 

4 


SCREW. BUT HO SELF U© SPLSX 

000250-1 



28 

1 

1 

HplaTe information 

1000622 



i if 

1 


1 Ir ATF-INFORMATION 

1000023 



26 

A/R 

A/R 

W 

LUBRICANT. IjOW CGRNT.G NQ5E 


kn-L -4343 

- 

25 

1 

1 

1 PLATE. O0-JT.F CATION 

ruoooei 



24 

8 

8 

8 

SCREW. BUT k. L SELF LHG 5R-.bcC 

1000250-0 



25 

12 

12 

1? 

IP 

SCREW. CAR SOC. Hu HEX 

.021400—is 



2i 

40 

40 

40 

SCREW. CAR SOC ~Q HEX 

0 01489-47, 



20 

2 

2 

? 

BACKING RREEORMEQ V wmg 

1000159-6 



19 

“j 


1 

qaCKlsia °REFORN€b. RNG 

1000159-5 





1 

| 

JALyE, PRESSURE, ASSY. 

000234 



17 

2 

? 

~P~ 

OOUF\JNGHALEQUlCK.DSCONNBCr 

1000135 



l« 

4 

4 

4 

SPRING. FASTENER 

IOOOI87_ 


_ 

18 


4 

4 

COVER. SPRING FASTENER 

•oooias 



14 

4 

4 

4 

SCREW, FASTENER 

1000186 



13 


1 

1 

-ReIquvW^module 

IOC 1475 



12 

t" 

1 

1 

PACKING, PUEPORMED/tD" RING 

000159-3 



II 

2 

2 

z 

PACKING. PREPORMEDfO" RING 

IOOOI59-t~ 



10 

T~ 

~r 

"a“ 

^CWNt.PREFORMED.T)" RING 

' 1000109 -a 



9 

i 

i 

i 

MT..CONN ASST JG* OUTER AW 

ICO1559.. 



a 


1 



' ,0CI558_^_ 



7 

~i~ 

i 

i 


iC00205 



6 


i 

i 


1001506-j;" ' 

___ 

_ 

” 5 

i 

i 

i 

CASE,COVER. FIXED 

000241 



4 



i 

CASE COVER MOVEABLE 

000082 



3 

~i~ 

i 

i 

OUTER AXIS. ASSEMBLY 

' i6Ci56u5ii 




— 


t 

MACHNE ASSY, CASE CENTER 

1000085 



_ 1 

— 




mm oa 

MONCAnON 

MTUMl 

mo 



Mg 

CM OftCMDTMN 

mtmwnm no 


oa win 

w. 


Bi 


LIST or PARTS ANO MATERIALS 



INERTIAL 
MEASURING UNIT 
ASSFMBLY 


IMCtCMrr CCNTCN 


1HUT I Q»_I 




n 


IJ 




r 


R 


•SiT 





MR* 
















































































































































m! 





3 



SEE NOTE SB 
4 PLACES 


REPLACES REV L WITH CHANGES 


REPLACES REViS.CN - WITH 
CHANGES TDRR 


H {REVISED TDTO. I4E39 - 



4 I 4 I 4 WASHER.CABLE CLAMP lOOQggS _ 

~T~ I I CLAMP, CABLE _ CP3220-6 

3 3 3 CL AMR CABLE _ 1000220-8 

-j-j~ IMU-CDU LOAD COMP MOO 1007550 r 

A/R A/R A/R ADHESIVE _ JQ1Q838- 

“j-i ~ INSULATION CASE HXCHR RH '1001477 

-- . ~ tNSUL ATION CASE HXCHR"LH 001 478 


~T~~T~ INTERGIMBAL SUB-ASS’Y I X OA OCH5Q6^l 

| _ _ OUTER AXIS ASS'Y _ 00*501-02 

T" 8 8 MJT a IJC RRISH-MCUMTH) IQ00076- 

A/RiA/R Tfi screw.CAP SOC *). hex _._ 

A/R A/R A/^ SCREWCAPSLF-LHGt SX PQPE> _ 

T7r a/R V^PGHTBftLANCE.OUTER CW L KXX)27Q 


A/R A/R [A/R V 
A/R A/R A/R V 
A/R A/R A/R V 
A/R A/R A/R \J 


FIGHT. BALANCE jOUTER GMKL >000268 
FIGHT. BALANCE OUTE MO GMBL. KXX' 263 
FIGHT. BALANCE MO. GM6AL OQG262. .. 


A/R 

A/R 

a/rIweghY balance S/m 

_fc00|60 _ 

A/R 

A/R 


WEGHT. BALANCE 5/ 

/M 

N000259T 

A/R A/R 


WEIGHT. BALANCE S/ 

^M 

1000258 

STr 

S7r 

A^ 

WEIGHT. BALANCE 5/ 

^M 

11000214 

t/R A/R 

aa 

WEIGHT BALANCE 5/ 


tpoos.i.? 

~IT' - 

1 

— 

OUTER AXIS ASS'Y 


1001501-021 

~T~ 


TIT 

CASE.COVER.UPPER 


II00I566 

4 

"4” 

t; 

[SCREW, BUT HO SELF LMG 5PL 

SDdlCX)0250-l 


ee notes; a 

EE NOTE 6 42 
EE NOTES < 
EEN0TE6 4 
EENQTP ~ ! 
EE NOTE 6 J 
EE NOTE 6 J 
EE NOTE 6 ! 
FF MTTF 61 1 
EENOtE6|2 
EE NOTES M 
SEENOtFS p 
EEN0TF612 


9 8 8 

12 12 12 
12 12 12 
40 40 40 

2 2 ”F 


T Slate information! KXXX)22__ 

T ^LATE .INFORMATION _ 1000023 

75 LUBRICANT 0 OH CORN‘ S NOSE _ 

| PLATE. OENT.F CATION lOOQOg l 

8 W. BUT SELF-L HGSR^X jOOOgSOg. 

12 SCREW CAP SOC HO. HEX ,001460-18 .. 

12 SCREW CAP SOC ~0, HEX_.0 014 9?-: j_ 

W SCREW CAP SOC ^HEX ■OQl480-4\. 

2~ POKING.PREEORMEQ'0'WNG_ ;000 53-6 

T~ =ACKHG. PREFOPKED.^ R MS 00050:5 
I JWE. PRESSURE, ASSTY. 000234 

2_ CXXR^H AlP 3UK0 < D6C0NNBC T lOCX>35___ 

4 SPRING, FASTENER _]OOOl87_ 

~4~ COVER. SPRING FASTENER 1000185 
4 SCRE W. FASTE N ER IOOOI88.. 

J_ J^foLV^^QQi&.t _ C0I4 - ’? 

I FWCKINC .PKFORMC O. ^RINS _ COOI59-3 

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I CASE£OV£R. MOVEABLE _ OO OC82 

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DRAWING NUMBER 
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WHEEw TYPES 
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jI GRAPHMO _ 

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vewE 

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■ SEE. NOTE, ft 



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L INTERPRET QRAA/VY6 N ACCORDANCE VMTM ML-D-70327 
Z ASSEMBLE $ TEST PER REQUPEACNT5 OF ATP 1000001$ FTM 1000201 
3L SCREW TORQUE REQUIREMENTS ±7* 

A. IQO MLBl 
a 5.o n. La 

C 2.0 IN. La AT FINAL SEATNQ NOT TO EXCEED ID N. UL WHLE ENGAONG PINS 
Q85.0 MLa 

E. 70.oriLa 

F. 65.0 IN. 13. 

G3Q.0 Ml_a 

4 MARK CHARACTERS^HIGH COLOR BLACK PER NO 1002019 AT- LOCATIONS SHOWN.' 

5. ENGRA€ CHARACTERS $ HGH ANO FILL, OOUOR BLACK PER NO 1002019 

6 BALANCE WEIGHTS ANO NUTS TO BE SELECTED FROM APPLICABLE DRAWINGS ANO 
INSTALLED PER ATP1000201. SELECT SCREWS FROM CHART 

7. USE DRAWING NUMBERS :?QOQie GHVBAL ASSEMBLY OUTLtC AND 1000017 

WIRING DIAGRAM FOR REFERENCE _ „ _ 

8. PROTECTIVE CCAEF.El_ECT.NASA DRAWING NO. 1001495,PROTECTIVE CCJ/ERUCOOLNYL 

^A DRAWiNGNO.lOOM^4, MOUNTING PAD COVERS, NASA DRAWING NOS 100(460,1001464<100461 

raijccAND imu oinTT on gumminn-n rmrrnmift rr be removed only 

WHEN REQUIRED DURING TEST AND INSTALLATION,OR TO PROVICE HEATER POWER 
m iNFRTlAi COMPONENTS. USE SELF LOCKING SC REW S. NASI35C04LL4.0R EQUIV, 

TO SK^ I^4%^C^I^TW MOUNT.ASSY7S(T)Ak)®• HtMOVE PTOTKTIvE COVER 

MOUNTING SCREWS AND CABLE IMMEDIATELY PRIOR TO INSTALLATION ! 

9 SECURE BALANCE WEIGHTS,ITEMS (3fe)THRU(40) TO GIMBALS WITH SCREWS PER 
’ SELECTION CHART, ANO ITEM ©AT REQUIRED LOCATIONS ON MCOLE AND OUTER 

GIMBALS. SEE VIEW E FOR TYPICAL INSTALLATION DATA. CAUTION: DO NOT NSTALL 
ITEM(35) IN LOCATIONS THAT WILL PREVENT FREE ROTATION OF GIMBALS. 

10 TEMPERATURE OF ASSEMBLY - MUST BE MAINTAINED BETWEEN I20*F ANO I40*E 
PULSED INTERGRATING PENQULJM.NASA DRAWING NO.000013. MUST BE RECALIBRATED 
IF TEMPERATURE EXCEEDS THESE LIMITS. GYRO PREALIGNED ASSY.,NASA DRAWING NO. 

1000012 MUST BE RECALIBRATED E TEMPERATURE EXCEEDS 40*F*T0 IG0*F RANGE. 

II. STAMP OR ENGRAVE SERIAL NUMBERS OF I RIGS. NASA DWG. NO. 1000012, ANO PIPS NASA 
NQ.1000013 IN APPROPRIATE BLOCKS PER NO 106209 
12 ITEM ( 49 ) TO BE SELECTED B MAINTAINED IN CONJUNCTION WITH THIS ASSEMBLY. 

ITEM (49) TO BE ASSEMBLED ON 1007152 WITH 13TO 17 IN-LB OF TORQUE AT I.S.S LEVEL. 

SELECT ITEM (49) FROM TABLE I 

a BONO ITEMS © a © TO ITEM(T)WITH ITEM ©. COAT MATING SURFACES OF ® © a(D 
WITH (48) BEFORE ASSEMBLY 

14 FOR SPARES PROCUREMENT ,THIS ASSEMBLY MUST MEET THE REQUIREMENT OF PS1000701 



■—MARK J2 
SEE VEW C-C TYP 


SEE VEW C-C TYP 


CD® 

2 PLACES 


-CD 

2 PLACES 
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SHOWN WITH NO INSULATION 


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VIEW 


F-F 


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Eh- 



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42 



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WEIGHT. BALANCE.OUTER GMBAL 
//EIGHT. BAlANCE.OUTER GIVBAL 



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41 


a/R 

000270 


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40 1 

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A/R 

A/R 

000268 


3EE NOTEC 

39 



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wf ight. bal anqe out i via gmbl. 

000263 


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000262 


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3/ 

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000261 


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36 

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1000260 

000259 


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35 

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v/eight. balance s/m 


33 

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000258 


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a 7 r 

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1000214 


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32 


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1 


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31 


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1001501-021 



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| 



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MOTES 

l INTERPRET DRAWING M ACCORDANCE WITH ML-0-70327 

2. ASSEMBLE $ TEST PER REQLHREMENTS OF ATP lOOOOQi^ FTM 1000201 

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a 5.0 m La 

c. 2.0 in. La at final seatng. not to exceed id n. La whle engagng pins 
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E. 70.(7 IN. LB 

F. €5.0 IN. La 
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INSTALLED PER ATP1000201. SELECT SCREWS FROM CHART 
USE DRAWING NUMBERS QMBAL ASSEMBLY OUTLINE AND 1000017 

WIRING DIAGRAM FOR REFERENCE 

- PROTECTIVE COVER,ELECT,NASA DRAWING NO. 1001495, PROTECTIVE COVER .COOLANT. 

NASA DRAWING NO. 1001494, MOUNTING PAD COVERS, NASA DRAWING NO.’S 1001460,1001464^1001461 
lOOI465. 4NB- t MU SM A P-ON BEL LOWS.NASAO RAWING NO. 1 900602 JO BE REMOVED ONLY 
WHEN REQUIRED DURING TEST AND INSTALLATION,OR TO PROVIDE HEATER POWER 
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TO SECURE 1001495 TO CONNECTOR MOUNT. ASSY.*S(T)AfO(T). -r MOvE PRJTFC ii. E COVER 

MOUNTING SCREWS AND CABLE IMMEDIATELY PRIOR TO INSTALLATION 
9 SECURE BALANCE WEIGHTS.ITEMS (36) THRU (40) TO GIMBALS WITH SCREWS PER 
SELECTION CHART, AND ITEM(43)AT REQUIRED LOCATIONS ON MCDLE AND OUTER 
GIMBALS. SEE VIEWE FOR TYPICAL INSTALLATION DATA. CAUTION: DO NOT INSTALL 
ITEM(53) IN LOCATIONS THAT WILL PREVENT FREE ROTATION OF GIMBALS. 

10.TEMPERATURE OF ASSEMBLY - MUST BE MAINTAINED BETWEEN I20°F ANO I40*E 

PULSED INTERGRATING penduljm,nasa DRAWING NO. 1000013. MUST BE RECALIBRATED 
IF TEMPERATURE EXCEEDS THESE LIMITS. GYRO PREALIGNED ASSY.,NASA DRAWING NO. 

1000012 MUST BE RECALIBRATED IF TEMPERATURE EXCEEDS 40*F*T0 I60*F RANGE. 

!!. STAMP OR ENGRAVE SERIAL NUMBERS OF I RIGS, NASA DWG. NO. 1000012, AND PIPS NASA 
NOIOOOCM3 IN APPROPRIATE BLOCKS PER NO 1002019 
12.ITEM (49) TO BE SELECTED 8 MAINTAINED IN CONJUNCTION WITH THIS ASSEMBLY. 

ITEM (4D TO BE ASSEMBLED ON 1007152 WITH 13TO 17 IN-LB OF TORQUE AT I.S.S LEVEL. 

SELECT ITEM (49) FROM TABLE I 

13. BOND ITEMS (46) 8 (37) TO ITEM(T)WITH ITEM (48). COAT MATING SURFACES OF (46) © 8© 

WITH (48) BEFORE ASSEMBLY 

14, FOR U-ARES PROCUREMENT .THIS ASSEMBLY MUST MEET THE REQUIREMENT OF PS\OOCEO\ 




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010861-6 ! 

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4 

4 


>CREW,0UT. HD,SELF LKG. SPL SOq 100250-12 | 

_J_ 

55 ^ 

A/R 

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lAPE.ADH.ELEC. 1/2 WIDE 


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021405 

c 

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5 il 

4 

4 

4 

WASHER.CABLE CLAMP 

000223 


52 

1 

1 

1 

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000220-6 


51 

3 

3 

3 

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000220-5 



50 

1 

1 

1 

MU-CDU LOAD COMP MOD 

007550 


SEE NOTE 12 

49 

A/R 

A/R 

A/R 

ADHESIVE 

010838 


SEE NOTE 13 

48 

1 

1 

1 

NSULATION CASE HXCHR RH 

001477 


3EENOTEI3 

47 

1 

1 

1 

NSULATION CASE HXCHR LH 

1001478 


SEE NOTE 13 

45" 

1 

_ 

_ 

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KXM50£T 



45 


_ 

_ 

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001501-031 


I 44 

_ 

ft 

R 

MJT. CLWCH. FLUSH-MOUrvnED 

0000764 


SEENOTEe! 43 

aTr 

A/R 


SCREW CAP SOC »-0. HEX 

001489 


SEE NOTE 6 

42 

A/R 

A/R 

A/ft 

SCREWCAPSLFlhGiSOC kjpo 

001488 


SEE NOTES 

41 

A/R 

A/R 

A/ft 

vA^OHXBALANCE. XITER gmbal 

000270 


5EENOTE6 

40 I 

A/R 

A/R 

A/ft 

VaGHT. BAJWVCE.OLTER GMBAL 

000268 


SEE NOTE G 

39 

A/R 

A/R 

A?R 

WEIGHT, balance OUTE'MOl gmbl. 

000263 


5EEN0TE6 

38 

A/R 

A/R 

A/ft 

^aGHT. BALANCE MlQ GMBAL 

000262 


SEE NOTE 6 

TF 

A/R 

A/R 

A/ft 

WGGHT, BALANCE MlQOMBAL 

000261 


SEE NOTE 6 

38 

A/R 

A/R 

A/R 

a£ChT. balance S/m 

1000260 


SEE NOTES 

35 

A/R 

A/R 

A/ft 

weight. BALANCE S/m 

00025$ 


SEE NOTE 6 

34 

A/R 

A/R 

A/ft 

WEIGHT. BALANCE S/M 

000258 


SEE NOTES 

33 

A/R 

A/R 

A^ 

WEIGHT, BALANCE s/m 

000214 


5EEN0TF6 

32 

A/R 

A/R 

A/ft 

weight, balance s/m 

000213 


?EE NOTES 

37 


1 


OUTER AXIS ASS'Y 

001501-021 



30 

1 

_ 

IT 

CASE, COVER.UPPER 

1001566 



29 

4 

4 

” 

SCREW, BUT HO SELF LHD SPL90C 

000250-1” 



28 

1 

1 

1 

slate information 

1000622 



2 / 

1 

1 

1 

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1000023 



2b 

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V1L-L-4343 


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1 

1 

1 

PLATE. 00 JTF CATION ! 

1000021 _ 



24 

4 

4 

4 

oCREWBJT -v.SELF LM3SR3a 

100025c-A 



25 

12 

12 

T2 

SCREW CAP SOC HQ F€X 

4.101489-iB 



22 .. 

24 

12 

12 

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,0014 39-4 3 



21 

28 

28 

28 

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''01489-4?, 



20 

2 

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18 

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1 

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PRESSURE, ASSY. 

000234 



17 

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4 

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1000168 



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NOTES 

1 INTERPRET QRAA/TJG IM ACCORDANCE WITH 1^.-070327 

2 ASSEMBLE $ TEST PER REQUREMENT5 OF ATP iOOOOOi< FTM 1000201 
2 SCREW TORQUE REQWREMENTS tl% 

A. IQO MLB. 
ft 5.0 MLR 
C I JO Mia 
Q85.0N.l_a 

E. 70.OMLB 

F. 65.0 Ml_a 
GsaoMia 

H. 3.5 IN lB* 

4 MARK CHARACTERS^7HIGH COLOR BLACK PER NO 1002019 AT-LOCATIONS SHOWN. 

5. ENGRA/E CHARACTERS $ HOH ANO FEL.OOUOR BLACK PER NO 002019 

6 . BALANCE WEIGHTS ANO NUTS TO BE SELECTED FROM APPLICABLE DRAWINGS AND 
INSTALLED PER ATPlOOOOOL SELECT SCREWS FROM CHART SEE NOTE 9 

7. USE DRAWING NUMBERS lOQOQiS OMBAL ASSEMBLY OUTUNE AND 021412 
WIRING DIAGRAM FOR REFERENCE 

8 . PROTECTIVE COVER.ELECLNASA DRAWING NO. 1001495,PROTECTIVE CCVERjCOOLANt _ 

NASA DRAWING NO. 10014^4, MOUNTING PAD COVERS, NASA DRAWING NOS 1001460,1001464 <1001461 
I001465l 4N&TM U SNAP^ N=B B.U?waNASA D R AWING N04 9 Q0 8 0g JQ BE REMOVED ONLY 

WHEN REQUIRED DURING TEST AND INSTALLATION,OR TO PROVIDE HEATER POWER 
TO INERTIAL COMPONENTS. USE SELF LOCKING SCREWS, NASI35C04LL4,OR EQUIV, 

TO SECURE 1001495 TO CONNECTOR MOUNT. ASSY’S (7_)AMD(T) SCREWS NOT TO PROJECT BELOW 

:/Gw\T;NG SvJWACE ON(T)® (jD REMOVE PROTECT IVECOVER 

MOUNTING SCREWS AND CABLE IMMEDIATELY PRIOR TO INSTALLATION 1 ' 

9. SECURE BALANCE WEIGHTS.ITEMS (3?) THRU (40) TO GIMBALS WITH SCREWS PER 
SELECTION CHART,8 (56) 0R(5T)AT REQUIRED LOCARONS ON MCDLE AND OUTER 

GIMBALS. SEE VIEW E FOR TYPICAL INSTALLATION DATA. CAUTION: DO NOT MSTALL ITEM (5S) OR 
. ITEM(j3)lN LOCATIONS THAT WILL PREVENT FREE ROTATION OF GIMBALS. 

10. TEMPERATURE OF ASSEMBLY - MUST BE MAINTAINED BETWEEN I20*F ANO I40*E 
PULSED INTERGRATING PENOULJM,NASA DRAWING NO.000013. MUST BE RECALIBRATED 
IF TEMPERATURE EXCEEDS THESE LIMITS. GYRO PREALIGNED ASSY.,NASA DRAWING NO. 

1000012 MUST BE RECALIBRATED IF TEMPERATURE EXCEEDS 40VT0 I60*F RANGE. 

£1. STAMP OR ENGRAVE SERIAL NUMBERS OF I RIGS. NASA DWG. NO. 1000012, AND PIPS NASA 
NCUOOOOI3 IN APPROPRIATE BLOCKS PER NO IO02OI9 
IJL ITEM (49) TO BE SELECTED 8 MAINTAINED M CONJUNCTION WITH THIS ASSEMBLY. 

ITEM ® TO BE ASSEMBLED ON 1007192 WITH OTOrr M-L0 OF TORQUE AT I.&S LEVEL. 

SELECT ITEM (?9) FROM TABLE I 

IS. BOND ITEMS © 8 © TO ITEM(T)WITW ITEM ©. COW MATING SURFACES OF ® ® 8CD 
WITH (48) BEFORE ASSEMBLY 

14. FOR SPARES PROCUREMENT ,TH\S ASSEMBLY MUST MEET THE REQUIREMENT OF PSlOOOEO* 
». TA®E ITEM (g) SHALL BE USED AS REQUIRED TO RESTRICT MOVEMENT OF THE HARNESS IN THE CABLE CLAMP 


-MARK J2 
—. VCW C-C TYP 



SHOWN WITH NO INSULATION 


K. COOLANT PASSAGES SHALL MEET THE CLEANLINESS REQUIREMENTS OF ND1002223 
WHEN ITEMS(j6XjI)a(25)ARE ASSEMBLED TO CASE.ITEMfO 



l? 


II 


_J0 



9 















3 




_ * wtvmom _ 

ITM | OOCITTIOW 

^ 'replaces REVpSiON L with 
CHANGES TDRR -307 
N IPEY'SED TDRR 1«?39 
P 1 REVISED TDRR 14673 
R REVISES ^DRR 5^:6 

S REVISES TDRR 16808 _ 

T 'REVISED TDRR 680* _ 

U [REVISES TDRR 17490 _ 

V REVISED TDRR 2234-4_ 


!- NUT. CLINCH PLAIN _10108 61-6 

[~4~ S CREW.BUT. HD.SELF LKG.SPL SOQ 100250-12 ] 

‘a/r'tAPE.ADH.ELEC. 1/2 WIPE ._£ 

Ia/R IwEIGHT.BALANC S S/M 110? 1405 i_ 


_SEE NOTE® 56 

ZZ“Z_ ' _.J» 

L-1-15126 TYPE ACT 54 


WEIGHT,BALANCE S/M 

10? 1405 

9EEN0TE6 53 

WASHER,CABLE CLAMP 

000223 

1 52 

CLAMP. CABLE 

1000220-6 

1 51 

CL AMR CABLE 

,000220-5 

50 

IMU-CDU LOAD COMP MOO 

IOC7550 

SEE NC T Ei2j 49 

ADHESIVE 

1010838 

SEE NOTE 13) 48 

INSULATION CASE HXCHR RH 

001477 

SEE NOTE® 47 

INSULATION CASE HXCHR LH 

001476 

SEE NOTE I3| 4C 

INTERGIMBAL SUB-ASSY IX OA 

001506-2 

1 45 

OUTER AXIS ASSTf 

i00l5bl-03l 

_1 44 

NUT. CUKICH. OLUSHW0JNTED 

10000764 

seenotesNl 


A/R A/R A/P SCR EW. CAR SOC *3. h£X 1001 489 

A/r|a/R V5 SCREWCAPSLF-LKGt S O C t-Q 1001488 
a /r I a/r a/5 alight.bal ance,xiter gmbal_ 00) 270 
A/R A/R A/PWBGHT,BA>J>fJ CE t XTERGMBAL 1000268 
A/R A/R A A? WEIGHT. BALANCE OUTtMlQ CMBU '00 0263 
A/R A/R A/R ALIGHT. BALANCE MG GMdAL 000262 


A/R 

A/R A/R-A€CHt BALANCE 

5/M 

1000260 

A/R 

A/R A/E WEGHT. BALANCE 

S/M 

1000259 

A/R 

A/R A/P WEIGHT. BALANCE 

S/M 

1000258 

m/R 

A/R A/P A/EKjHT,BALANCE 

S/M 

I00o2i4 

A/R lA/R i A/Pi WEIGHT. BALANCE 

s7m 

k/C02i3 

- 

1 | - IOUTER AXIS ASS'Y 


11001501-021 

' 1 

- - tase, cover,upper 

IIO-I^OL 

4 

4 4 SCREW, BUT HO SELF LUG SPL9C 

q 000250-1 

mm 

!—— 


J 1000022 

11000023 

A/R 


RN-t-.^NOS 

9 

1 

till R_A T E. lOEN' E CATO 

N 

koc 02 l 


EE NOTE 6 , 42 
EE N0TE6 _4I_ 
EE NOTES 40 
EEn6te G | 59 
EE NOTES 1 36 
EENOIEfe 37 
iGNOTES 36 
EE NOTE 6 35 
EE NOTE S 34 
EEJMOTES 33 
GNOMES 32 
SNQTrSi 31 


•'RI MS_11000159 

T RIN G ~ . ,000155 
" RING 1000159- 

4 OUTER AM 1001559. 
UTER AXIS 001558 


" 01489 4?, 

ZooiS^H 

(000159-5 
000234 
I000135_ .. 

JO 00187_ 

1000185 ' 
IOOOI68 

1000159*3 
1000159 V 
1000159-a 


ry-SOT* —_— T 

CAae.covFR. fi xed 
CA9E;C0VER MOVEABLE ’ 

! OUTER AXIS. AS SEMB LY 
~ MACWNE ASSY. CASE CENTER 


000205-011 
1001506-1 ' 

CC024I__ 

00 0082 

~ rocigo ^sii 

1000085 


IIST Of PARTS AMO MATERIALS _ 

INERTIAL 

MEASURING UNIT SEI 
ASSEMBLY ^ 






























































































r 




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B 




TABLE l 


GYRO WHEEl. TYPES 

~ r ~ PART NO. 

3 s:mcnds 

1007550 -011 

! 2 3,'MCNDS 

1IC07550-02I 

I GRAPH MO 

1 

: SIMCNDS 

S1007550-031 

2GRAPHM0 


3 3RAPHM0 

ICO7550-04I 



NOTES 

l fyfTERFRET QRAWNG M ACCORDANCE WITH ML-D-70327 
Z ASSEMBLE $ TEST PER REQLHREHCNTS OF ATP * .wO £ FTM >000201 
a SCREW TORQUE REQUIREMENTS ±7% 

A. IQO MLJL 

a 5.0 m lb 

C. 1.0 N.LB 
D85.0 f\Ll_a 

E. TO.OMLB 

F. € 5.0 IN. La 
G 3 Q 0 IN. La 

4 MARK CHARACTERS^HIGH COLOR BLACK PER NO 1002019 AT. LOCATIONS SHOWN. 

5 ENGRA/E CHARACTERS \% HK3H ANO FILL. COLOR BLACK PER NO 1002019 


: BALANCE WBOTTS ANO NUTS TO BE SELECTED FROM APPLICABLE DRAWINGS AND 
INSTALLED PER ATPIOOOOOI. SELECT SCREWS FROM CHART SEE NOTE 9 


USE DRAWING NUMBERS XuO OMBAL ASSEMBLY OUTL*>E A/SCH02I4I2 
WIRING DIAGRAM FOR REFERENCE 

• PROTECTIVE COieT,EL£CT,NASA DRAWING NO. 1001495, PROTECTIVE CCVERLCOOLANt ._ 

NASA DRAWING NO. 1001494, MOUNTING PAD COVERS, NASA DRAWING NO^S 0bl460,1001464<1001461 

WHE^REQUI^D^URING ^^V^4ND f |^^SLUAT»0N^>R C T^F§^Scfe HEATER POWER 

TO INERT,A U COMPONENTS. JSE SELF LOCKING SCREWS. NASj35C04LL4,0R EQUIV,_ 

TO SECURE 1001495 TO CONNECTOR MOUNT. ASSY’S(7)AN0 (TT) SCREWS NOT TO PROJECT BELOW 


VOX^NG SURFACE ON (j7j 8 (IT, REMOVE PROTECTIVE COVER 
MOUNTING SCREWS AND CABLE IMMEDIATELY PRIOR TO INSTALLATION 


9 SECURE BALANCE WEIGHTS,ITEMS (3§)THHu(40) TO GIMBALS WITH SCREWS PER 
SELECTION CHART.8 (56)CR©AT REQUIRED LOCATIONS ON MCOLE AND OUTER 
GIMBALS. SEE VIEW t FOR TYPICAL INSTALLATION OATA. CAUTION: DO NCT INSTALL ITEM © OR 


ITEM© IN LOCATIONS THAT WILL PREVENT FREE ROTATION OF GIMBALS. 

L,TEMPERATURE OF ASSEMBLY- MUST BE MAINTAINED BETWEEN I20*F ANO I40*E 
PULSED INTERGRATING PENDULJM,NASA DRAWING N0.I000CI3. MUST BE RECALIBRATED 
IF TEMPERATURE EXCEEDS THESE LIMITS. GYRO PREALIGNED ASSY.,NASA DRAWING NO. 
1000012 MUST BE RECALIBRATED IF TEMPERATURE EXCEEDS 40*F*T0 IGOV RANGE. 

! . STAMP OR ENGRAVE SERIAL NUMBERS OF I RIGS. NASA DWG NOL1000012, ANO PIPS NASA 
NO.1000013 IN APPROPRIATE BLOCKS PER NO 1002019 


12 ITEM (49) TO BE SELECTED 8 MAINTAINED IN CONJUNCTION WITH THIS ASSEMBLY. 

ITEM (49) TO BE ASSEMBLED ON 1007152 WITH 13TO 17 IN-LB OF TORQUE AT I.S.S LEVEL. 
SELECT ITEM (49) FROM TABLE I 

13. BOND ITEMS © 8 © TO ITEM(T)WITM ITEM (48). COAT MATING SURFACES OF ® ® 8© 


viewE 

TYPICAL INSTALLATION 
SEE NOTE 9 



16. COOLANT PASSAGES SHALL MEET THE CLEANLINESS REQUIREMENTS OF ND1002223 
WHEN ITEMS flp(15)8(25)ARE ASSEMBLED TO CASE,ITEM(T) 


\ 


WITH © BEFORE ASSEMBLY 

14. rex ; - ARES PROCUREMENT .THIS ASSEMBLY MUST MEET THE REQUIREMENT OF PSIOOCEOV 

15. TAPE ITEM (54) SHALL BE USED AS REQUIRED TC RESTRICT MOVEMENT OF THE HARNESS IN THE CABLE CLA»#> 


l? 


II 



i ■ : - 7 — 


.IQ 


1 “ • 9 













3 


! „ REPLACES REVISION - W*TH 
* CHANGES T CRR - 
N [REVISED TDRR HJ39 I 

P REVISED TDRR 14673 ^ 

R RE VISED TDRR 15716 _[ 

S REVISED TDRR 16608 _H 

T REVISED TDRR I66C^_" 

U REVISED T DRR 1 7^90 

V [REVISED TDRR 2 : 34.4 | 3 

w BIASED PEA 23222 i 


-**<4 

ii- <*1-444 1 

ft' 


-rj> 

6 PLACES 
SEE NOTE 3G 



TOi 

K4/ 




m 









wot 

' /©O 





VIEW E-E 


VIEW A-A 


-SEE MOTE 30 
7 PLACES 


-SEE MOTE 3B 
4 PLACES 


REPLACES REV L WITH CHANGES 


NUT, CLINCH PLAIN_I0I086I-6. 

SCREW.BUT HD.SELF LKG. SPL SOC 10025042 
riAPE.ADH.ELEC, 1/2 WIDE ' 

? IwElGH T.BALAN CE S/M 172 1 405 

_TWASHER,CABLE CLAMP 1 100 0223 

j CL AMR CABLE_. lOC r 22C-6~ 

TcL'amR CABLE ” .IXC220-5 

flMU - CDU LOAD COMP MOD IICC7S5C 

?; ADHESIVE _ |lQlC839 _ 

INSULATION CASE HXCHP RH KOOI477 

“ INSULATION CASE HXCHR LH 001476 

_ INTERGIMBAL S UB-ASS'Y T)TOA 10015 06^2 
~ OUTER AXIS ASS^Y ~i0Ql50l-03l 

MUX CLFJCH.rLUSM-MOUMTED 100 00764 

l SCREW.CAP SOC K). HEX 1001489_ 

l SCREW C A P SLF-LHG, S OC Kjt-C* I00i488 


1001 501- 031 

"100 00764 

1001 489 _ 

X J001488 


A/P 'A^IQHXBALANCE.XITER GMBAL 1000 370 
A/P WEIGHT, BAlAN CE.QLTEP GIVBAl IQQQ268 
A/R WEIGHT. BALANCE OUT gMQ GMBL. '000263 


A/R 

iA/R 

A/RIWEOHT. BALANCE MlQ GTvbAL 

T60G262 

A/R 

IaTr" 

A/R 

WEIGHT, BALANCE MlQolMttAL 

TGG026. 

A/R 

A/R 

a/p|-a€Cht. balance S/m 

It 10260 

A/R 

A/R 

A/? 

weight balance s/m 

H0OO259 ^ 

A/R 

A/R 

A/R 

weight, balance s/m 

[1000250 

A/R 

A/R 

A/Q 

/VEKXT BALANCE s/m 

tiQuu24 

A/RIA/R 

A/R 

A/EiGHT. BALANCE S/M 

fcuujSO 

- 

1 

- 

OUTER AXIS ASS'Y 

JlOf 1501-021 

1 

— 

— 

"ASE,rrvEP,UPPER 


4 

4 


SCREW, BUt HO SELF LHG SPL93 

i 1000250-1 

1 

1 

"~P 

Plate information 

J 1 OOOO 22 

1 

1 

1 

PLATE .INFORMATION 

|l600623 

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w 

LUBRICANT uOv ‘ CORN *'.G NQ5E 

3 

1 

' 

1 

PLA T EJDEU'FCATlON 

JIC0002I 

4 


4 

►SCREW BuT ^.SELF lwgsrw 

Loogs&mS' 

12 

nr 

12 

SCREW cap SOC HD. HEX 

[. ''48? 16 


SCREW CAP SOC x_ _ 

■ SCREW CAP SOC -O. HEX 
R&CXJISJG. ^REFOPtvEu V PNG 
" ^Q<ls lG. =»R0^ OPf.'ED. J O' RWG__ 
^E, PRESSURE, ASSY. 

_ CCLP Jvla *-A_EQOCK, D6CONN0 

SPRING, FASTENER_ _ 

" COV ER. SPRING F ASTENER 
SCREW. F ASTE N ER 
_ VVfe^^MOD'JLE 

PACMNC. PREFORMED,^'JNN6 _ 
HACKING. PREFQHMEft't) RING 
'ACI0N6, PRE FORME D/0" RING 


MT.CONN ASST IGA OUTER AI9 IOOt**B. . 

MT. CONN A£ &T i- XX/TEB AXIS 001558 

1001506-1 

CASE,COVER. FIXED_ 000241 

_ CASEjCOVCR MOVEABLE 00 0082 

_ OUTER AXIS. ASSEMBLY I OC'501-Oil 

MACHNE ASSY, CASE CENTER 1000085 


_SEE NCTE6 56 

55 

- I-i5!26 TYPE ACT * 54 


BEE NCTE 2 4 
. GEE NCTE 3 4 , 
' see NOT a 
TsEE NOT' dT"? 


SEE NOTE e j~42 
£FNQTF6 | 41 
SEE-JQT EC 40 
JE MOTfX | 39 
SEENO r £6 38 
5EENJ IE6, 37 
5EEMOTE6 36 
3EENC7EO 35 
SEE NOTES' 34 
EE NOTE 6 _33 
5EENQTF 6 t~32 

BENOIT 6* 31 

_L?0 


■ 00I4 9S- 
' 01489 47, 

" 00015 9-6 
1000*59-5 
000234 
11000136 

•00010 7_ 

1000165 
10 00166 
100! 4^5 
OOOI50-3 _ 
IOOOI59-1 ~ 

" 1000159 - a 


ll015 000 IDLIOOISOOI*"' 


LIST or PARTS ANO MATERIALS _ 

INERTIAL -1 

MEASURING UNTT HsI 
ASSEMBLY —~ 







































































































1 SCREW SELECTION CHART | 

drawing NUMBER 

USED ON 

~-;-2 

STABLE 

member 

-3 

- T,- c -6 

. - r ,, ;:0G'438- 

Ml DOLE 

AND 

OUTER AXIS 

w - ;' 1 j 1001433-2 

14-0- 4 IC0I433-3 

■ 4 s' 3 '00)483-4 

.-1439 ( '00 488-5 

Oil j 02' 031 



*4B_‘ . 

~ yPES 

PART NO. 

3 3 \C' 

1007550-011 

' : GP-_ 

1007550-021 


1007550-031 

2 } PA— VIC 

1007550-041 


viewE 

typical installation 

SEE NOTE 9 


<*■ 


c 


A 



NOTES 


L INTERPRET ORAwJNG W ACCORDANCE WITH ML-O-70327 
Z ASSEMBLE $ TEST PER REQWPEMENTS OF ATP £ FTM 1000201 

3l screw torque requwements tr% 


A. 10.0 MLB. 

a 5.0 m La 
C. .0 M La 
QSb.0 MLE 
E. 70.0 M LB 
E 65.0 IN. LB 
6 30.0 IN. La 
H. 3.5 IN. lB- 

4 MARK CHARACTERS^7HIGH COLOR BLACK PER NO 1002019 AT LOCATIONS SHOWN. 


ENGRA/E CHARACTERS -jj HK3H ANO FILL. OOLOR BLACK PER NO 002019 


E BALANCE \A£GHTS ANO NUTS TO BE SELECTED FROM APPLICABLE DRAWINGS AND 
INSTALLED PER ATPlOOOJOl SELECT SCREWS FROM CHART SEE NOTE 9 

■ USE DRAWING NUMBERS - C3MBAL assembly Outlae and 1000017 
WIRING DIAGRAM FOR REFERENCE 

PROTECTIVE COVER.EUECT NASA OR AWING NO. 1001495, PROTECTIVE COVER .COOLANT. 

NASA DRAWING NQ.I00I4 9*, MOUNTING P A D COVER S, NASA DRAWWG NO.’S Obl460,1001464<I00I4GI 

’^Sf'^Sl^DUR^G = T^^AND 1 ^Si?AT!S5^^PR0VlciE 0 H?^TE^POWER^^ 

TO INERTiAl COMPONENTS. USE SELF LOCKING SCREWS, NASi 35C04LL4,0R EQUIV, 

TO SECURE 1001495 TO CONNECTOR MOUNT. ASSY’S (T)Ato(T)SCREWS NOT TO PROJECT BELOW 

VCwVTNC- SURFACE ON CO® GT REMOVE PROJECT 7EC0VER 

MOUNTING SCREWS AND CABLE IMMEDIATELY PRIOR TO INSTALLATION 


9. SECURE BALANCE WEIGHTS.ITEMS (3?)THPu( 40) TO GIMBALS WITH SCREWS PER 
SELECTION CHART.a (56', OR( 43 )AT REQUIRED LOCATIONS ON MOOLE AND OUTER 
GIMBALS. SEE VIEW E FOR TYPICAL INSTALLATION DATA. CAUTION: DO NOT M5TALL ITEM (x) OR 
ITEM (51) in LOCATIONS THAT WILL PREVENT FREE ROTATION OF GIMBALS. 


C,TEMPERATURE OF ASSEMBLY MUST BE MAINTAINED BETWEEN I20*F ANO I40*E 
PULSED INTFRGRATING PENOULJM,NASA DRAWING NO.000013. MUST BE RECAUBRATED 
IF TEMPERATURE EXCEEDS THESE LIMITS. GYRO PREALIGNED ASSY.,NASA DRAWING NO. 
1000012 MUST BE RECALIBRATED IF TEMPERATURE EXCEEDS 40*F*T0 I60*F RANGE 
f .. STAMP OR ENGRAVE SERIAL NUMBERS OF I RIGS. NASA DWG NO 1000012, ANO PIPS NASA 
NO1000013 IN APPROPRIATE BLOCKS PER NO I002CX9 


12. ITEM (49) TO BE SELECTED 8 MAINTAINED IN CONJUNCTION WITH THIS ASSEMBLY. 

ITEM (49) TO BE ASSEMBLED ON 1007152 WITH 13TO 17 M-LB OF TORQUE AT I.S.S LEVEL. 
SELECT ITEM (49) FROM TABLE I 

O. BOND ITEMS (46) 8 (37) TO ITEM(T)WITH ITEM (55) . COAT MATING SURFACES OF ® (47) 8 (T) 
WITH (48) BEFORE ASSEMBLY 


K FOR : - ARES PROCUREMENT .THIS ASSEMBLY MUST MEET THE REQUIREMENT OF PSlOOOZOI 
15. TAPE ITEM (54) SHALL BE USED AS REQUIRED TO RESTRICT MOVEMENT OF THE HARNESS IN THE CABLE CLAMP 



* COOLANT PASSAGES SHALL MEET THE CLEANLIICSS REQUIREMENTS OF ND1002223 
WHEN ITEMS(l6Xl9)8(25)ARE ASSEMBLED TO CASE,ITEM(T) 












MM 


M REPLACES REVISION L WITH 

CHANGES TDRR u3Q7 _ ** 

N REVISED TDRR t«539 rsc 

P 'REVISED TDRR 14673 V* 

R R EVtSED TDRR IS -7 6 " *,. « 

S REVISED TDRR 168 O 8 _ 

_T_ REV:SED TDRR 6607 _TZ . 

U REVISED TD RR 1 7430 _ V* 

V REVISED TDRR 2234.4. _ l3£ • 

W ' RE/'SEP ȣA TAR- 23222 * 7 \ 

Y {Rgy S£g 3£R - -RR - 2c '0 * 


ft-Sitf A i 
X- w ‘ 
y- 

I±r-444-^43 



/ SEE NOTE II 


VIEW F”F 


A/R A/R i A/R 
t A/R A/R [A/R 



- OUTER AXIS AS SEMB LY 

_ JZL OUTER Axi s ASSEMBLY _ 

_ — OUTER AXI5 ASSEMBLY __ 

_ - NUT.CLINCH PLAIN ' 1010861-6 

_ _4_SCREW,BUT. HO,SELF LKG.SPLSOC 100250-12 
MA/R TAPE.ADH,ELEC, 1/2 WIPE 

MA/R WEIGH^BALANCE S/M _ \J2 1 40S 

? 4 WASHER,CABLE^LAMP 1000223 

I CLAMP, CABLE_,100 0220-6~ 

1 3 ! C L AMR CABLE 11000220-5 

I IIMU-CDULOAD COMP MOO ~ ||QC 75 50 

M A/R ADHESIVE _ 1010838 

T I ! INSULATION C ASE HXCHR RH 1001477 

_ ~l | INSULATION CASE HXCHR LH 1001478- 

... ~ . INT ERGMBAL SUB-ASSY IX OA 1001506^2 " 


? A/R [ A/R AM 
I A/R : A/RjA/R 
A/R iA/R A/R 
A/ R A/R A/R 
TTa/R A/R |A /R 
A/R A/R A/R 
A/R a7b~|A7r~ 
I A/R A/R i A/R 
A/R A/R A/R 
A/R A/R A/R 
_ A, R A/R A/R 
A/R A/R A/R 


I 12 I 24 j 12 

126 1 28 1 2F 


REPLACES REV L WITH CHANGES 


1001501-Ofcl 

1P 0I5Q|-Q?r 

1001501-041 


HIL-I-I5I26 TYPE ACT 
_ I S ELNglES,; 


- OUTER AXIS ASS'Y 1iOQl5QlX)3l 

Q MJT. CLtviCM.FLUSH-MQUvnED llCXXX)76H 

_A/P 8CR EW.CAR SOC HQ. h£X ~h00 l4 89 
yg SCREWCA PSLF-LKX S OC Ed HExLqOI488 1 
4/^ /v€K3HT, BALANCE, X lTFR GMBaT10002~70 
jLP V/EIGHT, BALA NCE .QLTgP GM^J000268 
A/R WEIGHT. BALANCE OUTg MIQ GMBLJiQ00263 
A/R ALIGHT. BALANCE IVllQ QTv'dAL ['000262 
A/P WEIGHT. BALANCE MlO ( JMBAl IQCQ24I 
A/P /^GHtBALANCE S/M llC 00260 

A/P WEIGHT. BALANCE S/M~ H000259 “ 

A/P WEIGHT. BALANCE S/M [IQQ 0258 

yp /VEIGHT,BAL AN CE S/M 1000214. 

AEiGHT,BALANCE S/m bc02l3 

- OUTER AXIS ASS’Y |lPri50l-02l 

- '"ASE, rrvER,UPPER iiQ-|~PP 

_4 SCREW, BUT HO SELF LMS SPL90Q1000250-1 

I PLATE INFORMATION [1000022- 

I fo-ATE . INFORMATION IT000023 

VP LUBRIC ANT uO/ ■ w'JRN \S NO 53 

1 FLA T E.IDeiV F CATION kccoei 

4 pCREWBU-^ SElF LHGSR_^:d;UOG2SO-Q' 
12 SCREW CAR SOC. HO. HEX .i~ ~^ r - ,p 

i2 scre w cap soc> j -^:x ' _ 

2S SCREW CAR SOC -Q Hi^X ] C!48~9~ 

2 R^iNG.=PEFQPN£Qy RING 1X00159-6 " 

1 'Xkng. ^ pefqpMed, ”0" ring [000159-5 " 

i~i~ ^LVE,PRESSURE./^SV. n000234 

_ 2 _. <P>JNG'^C>jiCK,DiSCO^^ 

4 S PRING. FA STENER _ hoOOI0 7 _' 

4 COVER. SPRING F ASTENER jiboQl6S 
4 SCREW. FASTE N ER 1100 018 6 ~~~ 

.... 1 FESOLVfe^^MODULE ~K'0l4' r f 

J_ PACKING. PRf rOEMCD.Tr Ring _ llQOO 159*3 

2 PACKING.PREFORMED.7)" RING " ,1000159 1 ' 

2 PACKING,PWEFQWMED.-Q" RING 1000159-2 

I MT..CONN ASST J6A0UTD? AII9 |l00, K 59.. 

I MX CONN .YoS'Y l-XOCTER AXIS 1.001558 
J_ ' IC002-O00 “ 

_j_ ri r ssr^M' AWMeLV M 001506-1 

I CASE,COVER, FI XED 000241 

I CASE .COVER MOVE ABLE _ |:Cp0/'82 
I OUTER AXIS, A SSEMBLY |ICCI5?M5!I “ 

1 MACHNE ASSY, CASE CENTER MOrrv'q«= 


_ SEE NOTE12 ” 
_ SEE NOTE13 ■ 
' SEE NOTE 13 
ISEE NOTE 13 ~ 


H notes ; * 

NOTE 6 

SEFN0TE6 J 
JSEE10TE6 J 
SEENOTE^ I ! 
SEENOrgb l 2 
Denote e~ 3 

5 EE NOTE 6 3 
pEENQTE 6 3 
SEE NOTE 6 3 
gEEIM0TE6 J 
~gENQTF6 3 
SEE r jQTT 6 3 


LIST Of PARTS ANO MATERIALS 

INERTIAL 
MEASURING UNIT 
ASSEMBLY 


2 


*mx>nw 


WitnlE, 


'O \J\J 



















































































































10 


SCREW SELECTION CHART 
QRAWING NUMBER j USED~ON~ 


MIOOLE 

AND 

OUTER AXIS 



\ :HI [M ' THRU 


TABLE l 

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L INTERPRET DRAWING M ACCORDANCE \MTh ML-D-70327 

2. ASSEMBLE $ TEST PER REQUREMENTS OF ATP .U000oi$ FTM 0C020I 

3 SCREW TORQUE REQUIREMENTS ±7% 

A. IQO IMLB. 

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E.70.O INL LB 
c . 65.0 IN. La 
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ENGRA/E CHARACTERS HGH AND FILL. COLOR BLACK PER NO (002019 


: BALANCE W0OHTS AND NUTS TO BE SELECTED FROM APPLICABLE DRAWINGS AND 
INSTALLED PER ATPlOOC X)l. SELECT SCREWS FROM CHART SEE NOTE 9 
USE DRAWING NUMBERS - QMBAL ASSEMBLY OUTLINE AT® 1000017 
WIRING DIAGRAM for reference 

PROTECTIVE COVER. ELEC T,NASA DRAWING NO. 1001495.PROTECTIVE COVER .COOL ANT, 
NASA DRAWING NO. 1001494, MOUNTING PAD COVERS, NASA DRAWING NO?S 001460,100I4€ 



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SHOWN WITH NO INSULATION 


NASA DRAWING NO. 1001494, MOUNTING PAD COVERS, NASA DRAWING NO?S 001460,1001464<1001461 

WHEnP*REQUtH^AND^^^LLATI^OR^PROVIC^ H^ATER^POWE^^ 

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TEMPERATURE OF ASSEMBLY-MUST BE MAINTAINED BETWEEN I 20 °F ANO I40*F 
PULSED INTERGRATiNG PENDUL JM,NASA DRAWING NO.OOOCI3 MUST BE RECALIBRATED 
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1000012 MUST BE RECALIBRATED IF TEMPERATURE EXCEEDS 40*F*T0 lGO*F RANGE 
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ITEM (49) TO BE ASSEMBLED ON 1007152 WITH 13TO 17 IN-LB OF TORQUE AT I S.S LEVEL. 

SELECT ITEM (49) FROM TABLE I 

13. BOND ITEMS (46) 8 (57) TO ITEM(T)WITM ITEM (48). COAT MATING SURFACES OF (46)(47) 8(7") 

WITH (48) BEFORE ASSEM 8 LY 

K FOR ■ ARF_S PROCUREMENT THIS ASSEMBLY MUST MEET THE REQUIREMENT OF PS\OOCZO\ 
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■■ m\ 


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lESIHHH 


H 

fciEan 

iEa— 1 


MOTES 

1. KTTERPRET DR4A/AJG N ACCORDANCE \MTH ML-0-70827 

2. ASSEMBLE $ TEST PER REQUIREMENTS OF ATP IOOOOOI 

a SCREW TORQUE REQUIREMENTS *72 

A. IQO IN. LB 
a 50JNL i_a 
c as in. La 

Q INSTALL FINGER TIGHT 

4 MARK CHARACTERS $ HIGH COLOR BLACK PER NO 1002019 AT LOCATIONS 
SHOWN 

5 SOLDER PER ML STD 440 USING (g): WRE NSULATON SHALL 8E \MTMN 

06 OF SOLDERED CONNECTIONS _ 

6 USE DRAMNG NQ 000017 WRNS DIGRAM FOR REFERENCE 
TSECURE LEADS FROM (T) TO ( 77 ) WITH (|?J 

8 . TAPE ITEM (35) SHALL BE USED AS REQUIRED TO RESTRICT MOVEMENT OF THE 
HARICSS IN THE CABLE CLAMPS 


1001501 


10 


9 










































































































































































6 












































SEE MOTE 3A 
l€ PLACES 



(FOR-031) ®©®- 

IFOR -Oil-021) (34j^20Xl9Xl6> 
2 r 'i ACES 

SEE NOTE 3D 

SEE NOTE 3D 
(FOR -030 ®®CEh 
(FOR-OI1-021) C2Q®f6K 


\sEE NOTE 30 


2 PLACES YCP 




B TDRR l36S"0 
C TDRR 14543 

D ! TCRR <4544 _ 

E ! TDRR 16329 
F ! TD RR 16807 

G I TDR R I80S3_‘ 

H REVISED PER TDRR 23794 

J Revised Per to«r z * i-c 




1 .aJur 


SEE NOTE T 
2 PLACES 


SEE NOTE 4 TYP - 



-YU) 

4 places 
SEE NOTE 38 


SEf^NCfii 3C 

(Hh 


a 



(EK 

12 ^LACESV 
SEE NOTE 3A\ 


,0 0 

a_o_frv.„ 

r Fo 


- - - 'gE SISTOS BS *ND Xj6> 

- 2 - I WASHER, FLAT ROUND 


1010928- 3*7 
MS 15795 303 _ 


- SCREW CAR SOC HD HEX S.L. 1001488-1 

- HOUSNG ASSYOUTER GIMBAL PpP^?- 011 

* A/R TAPE.ADH. ELEC. PRESSURE SENS lEiteftEj* ' 

8 .A/ASHER , FL/VV^OUND_MS i^TDS-TO^ 

[— [ MIDOLE AXIS A SSEMBLY_1001502-031 

- iMI DDLE AXIS ASSEMB LY 1001502-021 

Ha/r! TAPE NY LON vVAXEO 

2 ttSUL ,SL EEVING ELEC . HT -SHRINK 010490-202 
2 I SLEE VING. HEAT SHRINK |Ot0490-078T 

10 ISCREW CAP SOC *) HEX ^ f 000110-302 

! SOLDER_ 5N6CMA RP2 

4 NSULAD0NSLEEVM3 _ 006776-19 

4 3CRE vyBOTM35ELP;LWG.SR^SX (00025042 ' 


MIL-T-113 TYPE P CL2. 3 

p/S LONG 3 


I SCPE WOPSELE HEX , HQ SOCNg i352C0»u < 

' 28 9CREWCAR ^ELE LK6, HEX, HQSOOiiC l352CO*ll4 
4 SC REWCAPSEUT U4 G. HEX. HQSOC H>5B52C02 Uj< ~ 
' 12 SCREW Cap SOC HD hex iodouo-7 

9 SCREW. CAP SOC HD HEX lQOO HQ-1 

8 NAASFER, GABLE CLANP 1100022 3 ~ 

4 CLA M? CA B LE _110002205 _ 

I C LAMR CABLE_ 10002204 

4 CLA M? C ABLE_ _ '000220-3 ~ 

I WIRING HARNESS^C*" Q.A. 1000124 

I \MRWG HARNESS *B" QA. 1000034 

1 CLI P OuTEfi 5M8AL _ 1000244 ~ 

2 a am? capacitor. oar. gimbal 1000235 

8 clam? bloneR 1000157 

4 COVER. BR ACKET, OONNSHOR JOOO143 

2 CCVEP CONN. MT, OUTER GMJAL' 1000239 ' 

' _2_ CAPACITOR, FIXED _ _____ 010264 ^381“ 

2 SATURA BLE, REACTOR 1000266 

1 REGULATO R, 28 VOlT DC _1007013 l 

' m elop er, variable speed nooog i 9 _ 

' “FjR J SE.PlGTAlL.SUBMIN |000I7CH0[ 

2 RESISTOR, FIXED ~Q|Q325-50C 


_ SEE NOTE S _ 
SEE NOTE 8 
SEE NOTE 8 


MIDDLE AXIS ASSEMBLY 


3GMBN. 1 000103 


LIST Of PARTS *N0 MATERIALS 

OUTER AXIS 
ASSEMBLY 


ICC; 501 




3 


2 



















































































































































2 




2 


80230 






























































































































































































































































I00I50I 















































* 













































































































1001502 











































































































































TQRR ■?? * 

TQWR >6400 ~ 
TDWR 16800 
TDBR (6607 
TDRR 16015 

Z0CQ7 

TDKR 204^5^ 


I INTEKG1MBAL SUB~A^YT)CMA|<0Qi5C6-3._ _ 

~ SCREW, SOC.HPHEX, S.L. 1001486-1 _ 

' HOUSING ASSY M.G. _ >000074-011 

: TA PL ADHESIVE ELEC M 

■ PRESSURE. SENSITIVE _ __ T 

INNER AXIS ASSY_1001903-031 

"INNER AXIS ASS'V _ <1001503-021 

INTERGIMBAL SUB-ASSY IX MA,001508-I _ 
1 fl Mtr,r IMH lj 1000220-5 

R SOLDER __ 5NG0>WARP 2[ C 

_ WASHER .CABLE CLAMP IOOQ2 2P _ _ 

_ CL AMP , CARLE _ 1000220- A _ 

CLAMP, CABLE __ 1000220^3 _ 

~ SCREW, CAP.Saf LKGlBEX HQiSOC itfSttS2CQ aU 
SCREW, CAP, SOC H P .HEX IQOOIIQ-I _ 
SCREW, PUT HD.SEIF LKfe.SPLSOC 1000250 • 12 
, SCREW, CAP.SELF LN&, HEX VO, SOC '*£>13S2C0*LIA 
I SCREW.CAP.SOCLUTUHEX _IQ QOnO-7 

■ CCVER, BRACKET CONN ICOQI4 P_ 

ADA PREAMP AVfr' M.G. >007853-0 l 

~ ACCEL ANGULAR DHTE RENTIATING,' 1000007 
~ INTERGIMPAL SUP ASSY IGX M.A. IQOOeOG 
- KTCRGIMPAL SUB-ASSY IX MA. CO 3^8-2 

INNER AXIS AVbY. _ .00.03-Oil 

HOOPING A«b5>V M.G._ 1000074 


3NCOWAPP2 QQ-P-571 

1000225,_ 

S D 22 Q-A _ 

0220-3 _ 

352CQ2U.1 ~~_ 


ust Of autts *wo materials 


Vide . 
see notc*M 


SEE NOTE a 14 

see hptl a Ts~j 


MIDDLE 

ASSEMBLY 















































































































































































WlRINS LEGEN# 


COND _ _ „ FIND „ jm]r _ 5EE 

NO C<X °* HQ. ***** 10 CHART 

> -1 WHITE _ A4-» kl-Z n 

1- 2 BLACK _ A4 - - A7- » O 

Z- l 'white A 5 -♦ ' AIO-I q 

2- 2 IBLACK AS - - 1 AIO- Z 0 


NOTES 

L INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70SE7 
£ ASSEMBLE f TEST PER REQUIREMENTS OF ATP 1000001 
S SCREW TORQUE REQUIREMENTS T7*JL 

A. 10.0 IN. LB 

B. 5.0 IN. LB 

C. S.5 IN. LB 

O. IQ lfeLLB ” 

4 MARK CHARACTERS E HIGH COLOR BLACK PER ND 10020ft AT LOCATIONS SHOWN 

5 SOLDER PER MIL STD - 440 USING (Tg) W1RE INSULATION SHALL BE WITHIN -OC. OP 
SOLDERED CONNECTIONS 

G. _ 

7. USE DRAWING NO. 1000017 WIRING DIAGRAM FOR REFERENCE 
«. TAPE ITEM (fl) SHALL BE USED AS REQUIRED TO RESTRICT MOVEMENT 
OF THE HARNESS IN THE. CABLE. CLAMPS 


































































-SEE NOTE Sft. 


SEE NOTE 5 
TZ PLACES 


D 

irw aryw 

SehdIH*, 


ianl 










































































































IBBBCDI 











































































































c 



SEE NOTE 


SEE NOTE 
4 PLACES 


SEE NOTE 
4PLACES 


B 


fTESt 

l INTERPRET DWG IN ACCORDANCE WTTH UL-D-70327. 
t. SCREW TORQUE REQUREMENT5: {*7%) 

A. KXO IN-LB 

B. 1.0 IN-LB 

C. 5.0 IN-LB 

3. ASSEMBLE per REQUIREMENTS of ATP 1000001 


A 


T 


* 















R ASSEMBLY 



INNER AXIS 
ASSEMBLY 













































































































































































































53 


DSEE NOTE 4 




SECTION D-D 

2 PUCES 


is 



SECTION C*C 
z rxb 


DETAIL F 

SCALE 4/1 

1001506-1 


x—® 

^ 4 PUCES 

/ 6 RACES 


x-CD 

—® 


-(36) SEE NOTE 4- 



WIRING LEGEND 


VUHT/BU* 

WT/owN/cy 

V*<TAEL/gBM 

WHT/0WM/6RN 

WHTjteWVttU 


•OOlSfl.S 


3 








































































7 


6 



SECTIONS E'E 
2 PLACES 


VIEW F-F 
TYPICAL INSTALLATION 
SEE NOTE 15 



view B- B 

NOTES: 

I. INTERPRET OWVMC IN ACCORDANCE WITH MA- 0-703*7 

E. MARK CHAWCTO g MSN COLOR *A* PW HO CMOS AT UXATION* 

* eccentwcity marks on both races or (T) to be aligned within b* or [-c-j and in tme erection 

or THE ARROW WHEN CD AND (t) AGE IN THE POSITIONSHOWN. APPLY THIN COAT OF (S) TO 
"'INSIDE DIAMETER OF (7J AND TO FAYING SIWFAC* OP (A) BEFORE ASSEMBLY. 

_;i APP.v (tf) ON THE THREADS OF ( j£) OR (53) BEFORE ASSEMBLING — 

A IDENTIFY USING DRAWING NOyRETASION LETTER, MRWCTUGR S SA SOL ♦ SERIAL HO. ON (J_/ f 
nmtchmg SERIAL NO ON (T) AT' THE indicated locations per NOTE 2. 

* SCREW TORQUE REQUIREMENTS £ 1% 

'By C-^ 40 IN. LB. 

(0) 103 Si LS 

(tp®©®® SOBLLB. 


WEST A-. 


Ce^C 2 S')( 2 c) s.§ i» 

7 SOLDER ALL LEADS FROM (T)^(4) TO LOWER SECTION OP APPROPRIATE TERMINAL PEI? MIL-STD-440 _ _ 

SOLDER ALL OTHIRLEADS TO EITHER UPPER SECTION or APPROPRIATE TERMINAL OR (jTj.® * ® 
PER mStD- 440 USING (3) . WIRE INSULATION SHALL BE WITHIN .OS OF SOLDERED CONNECTIONS. 

* MEAT SHRINK SLEEVING QN .TElST® SOFTER ASSEMBLY 

P. CAUTION*. SO NOT SEPARATE STUB SHAFT (£) FROM HOU SING BEARMSORREMOA^E 
TDRQUS MOTOR (T) WITHOUT FIRST ASSEMBLING FEEFER TO TONGUE MOTOR • 

A MAXIMUM ALLOWABLE TDRM * OBrlN. _ 

14. mmhpX l TEST PER THE REQUMBMENTS OF ATO P OOOOG. 

; ^m.SZXS'ZZm *CE%*** W Ttsr $ NSP€CTWM. 



imt 


SEE NOTE 4 


5 



DETAIL F 

SCALE 4/1 


1001506-1 



NO. OP LEAPS 1 NOt OP FULL TURNS MIN | NO.OF FULL TURNS MAX 











2 places 


mm? 


4 WRS 


36)SEE NOTE 4 



semoN D-D 

2 PLACES 


DETAIL F 

SCALE 4/1 

1001506-1 






<56) SEE NOTE 4 





X /V 

•»» 


V 


SECTION C-C 

2 fMCES 




WIRING 

LEGEND 

COHO 

NO 

COLOR 

'w* 

FROM 

u>-\ 

KD 

41 

PB-F 

*«-* 

BLK 

53 

P8-C 

67 

vwVreo 


se-^KT/Rcn" 

^6S 



w-wktMk 

49 

TEL 

42 

BB-P2 

?o 

VWT/VCL 


SB-wmt/vkl 

71 

VKHT/BUi 


BB-WHl/BUJ 

72-1 

vwt/o*w7©T" 


BO-PI 

72-2 

WHT/Vel/GW 


BOPS 

73-/ 

WHT/oRN/WN 


B0-P2 

73-2 

whtAx^Vvel 


BB-fH 

rt 

RED 


BO-PEP 

7S 

BJl 


BB-MX 



a » shld em 

39 SHIP 34 

39 SHIP 49 

39 SHLD 4T 









































































pp 


view F-F 
typical installation 

SEE NOTE 13 



view B- B 


notes: 

I. INTERPRET OMMN6 IN ACCORDANCE WITH MIL-D-703*7 

&. MARK CVOIMCTERS g HEN COLOR SUCK PER *>WWO» AT LOCATIONS 

SHOWN __ _ ,__ 

3 eccentricity marks on both races or (T) TO BE aligned WITHIN s* OF l-C- 1 ANO IN THE direction 
or THE ARROW WHEN QD AND CD ARE IN THE POSITION SHOWN. APPLY THIN COAT OF (£2) TO 
inside diameter or (Jj AND to faying surface or (T) BEFORE assembly. 

4. AP = _v (I?) CN THE THREADS OF (jP) 0R (ID BEFORE ASSEMBLING 

3 IDENTIFY USING DRKWW6 NO.,REVISION LETTER, MANUFACTURERS SYMBOL i SERIAL NO. ON Qj 4 
WSTCHNG SERIAL m ON (T) AT THE INDICATED LOCATIONS PER NOTE 2. 

4 SCREW TORQUE REQUIREMENTS t 1% 

QDdD *0 IN. LB. 


( 23 ) N US 

dD®©®® SO Hi LA. 

® S * # * 13 

1 SOLDER ALL LEAD® FROM (T) £(4) TO LOWER SECTION OT APPROPRIATE TERMINAL PET? MIL-9TD-<440 
MSI NO (5$). SOLDER ALL OTHER LEAD® TO EITHER UPPER SECTION OF APPROPRIATE TERMINAL OR GD,® 
PER M1L-STD- 440 USING (*•) . WIRE INSULATION SHALL BE WITHIN OS OF SOLDERED CONNECTIONS. 

MEAT SHRINK SLEEVING ON ITEMS(47)a(48) AFTER ASSEMBLY 

CAUTION: DO NOT SEPARATE STUB SHAFT FROM HOUSING BEARING (T) OR REMOVE 

TORQUE MOTOR © WITHOUT FIRST ASSEMBLING KEEPER TO TORQUE MOTOR (±). 

MAXIMUM ALLOWABLE TORQUE S Ol.'IN. 


USE CHICAGO STITCH LACING N AREAS WOCATCD. 

PROTECTIVE GAP, NASA OWE NO BOMBS,TO BE REMOVES OHTjAS NECESSARY FOR TEST $ MSPEOION. 




























































































































SECTION D-D 

Z PU«ES 


SECTION C-C 

2 PUCES 


JtH 

a 


<36) SEE NOTE 4 


—CIZ) 

0 PUCES 

—<g) 

X PUCES 

—® 

4 RACES 

f B2~ 

V 4 




- 

WRING 

LEGEND 


w 

COLON 

'*s? 

FROM 

TO 

44-1 

f«D 

41 

P0F 

B4PI 

**-* 

BLK 

19 

r+c 

BSP3 

47 

whi/rbd 


R8-WKTAM6 

ss-n 

44 

rw/wt 



‘1S4S 

<9 

TEL 

42 

a-P2 

BB4» 

70 

wwA/cl 


IS-WITT/ML 

IMS 

71 

wr/blu 



BSfH 

72-1 

WWT/ORN/0T 


BO-PI 

IMF 

72-2 

WMT/YEV./SRH 


BOPS 

C2-44 

75-/ 

WMT/o«»V 5RN 


SOPS 

1242 

73-2 

VMiT^ftVVtL 



E24* 

ft 

RED 


SO-PIS 

WL 

7T 

_ SkS _ 


SOMA 

_ *»» 

74 

TEL. 


s^tcl 

im 

77 

BLD 


BOSUI 


74 

VMT/SRUBUi 


n-t 


79 

**n/*LWf 


Ifr* 

I24» 


*CC!*Oe 


34 SHLD 24 

34 3HLP 44 

39 SHLD 49 

39 1HLO 4T 


I Ltll l 

1*7711 


















































































































35) SEE MOTE 4 




SECTION 0 0 


SECTION C’C 

2 PLACES 


DETAIL E 

SCALE 4/1 

1001508-1 


4 PLACES 



■r 


-SEE NOTE 2 FTP 


i)nc MOVED 




SEE NOTE 2 TVP 


VIEW SHOWN WITH ITEM © REMOVED 


1001508-2 


VIEW SHOWN WITH ITEMS 4 (ED R EM OVE0 


i 1001508 TbTT 


>0015 02 |0 LV00I500] 

•Kit MA’ 


1 

TT 

RING FOAM “ IIOOI5I5-2 I 



59_ 

_ 

i 

SPACER, 1' 

ooisa3 I 



68 

_ 

i 

DETAINER, RING, FRICTION (MODI 10015 £4 



57 

_ 

i 

,HAFT, STUB 1/ MIDDLE AXi4(M«|IOOI5 - 2l 



56 ^ 

2 


NS SLV ELEC HEAT SHRINK 1010490-180 


V4U»..... 

55 


i 

sHLD t GROUND ASSY 11000020-2 



54 



5HLD$ GROUND ASSY 1000020-1 



53 

2 ’ 

2 

5CR FLAT HD SELF LKG jlOOO 104-3 



52 

V - 

3 

SCR BUT HD SELF LKG 1000250-13 


_____ 

51 


1 

Limit switch m.a. Iiooisso 



50 

13 

IS 

MSULAnON, SLEEVmS. ELEC. 

00b77b- lb 



It 

A/R 

a£ 

TAP= , NYLON, WAXED 


MtL-T- "713 

t < r c_ 2 

46 

A/R 

1 

1 

A/R 

grease, lub(beacon 1*3) 


ML-6- 

3278 


47 

1 

BRACKET, RETAINING 

WIRE ELEC. TYPE E-28 ORN 

001589 

010416-4 


2D*TOTXL Uft 

4* 

43 

1 


WIRE ELEC. TYPE E-28 VIO 

1010416-8 


B'TOTAL lb 

44 

1 

1 

WIRE ELEC TYPE E-28 BRN 

1010416-2 


30* TOTAL LG 

*L 

1 

1 


1010416-6 


20*TOTAL Uo 

42 

1 

1 

WIRE ELEC. TYPE E-28 BUJ 

1010416-7 


5'TOTAL LG 

41 

1 

1 

WIRE ELEC, TYPE E 28 GY 

1010416-9 


i^TOTAL UG* 

A , 



WIRE ELEC TYPE E-28 YE_ 

WIRE elk; type E-28 RED 

1010416-5 


3'TOTAL LG 

?*. 1 

1 

1 

1010416-3 


jb'tutal lg| 

36 


1 

WIRE ELEC TYPE E-28 WHT 

1010416-10 


0* TOTAL Uft 

JZ- 


1 

WIRE ELEC, TYPE E-28 BLK 

1010416-1 


12** TOTAL LC 

36 

A/R 


ADHESIVE, GOODYEAR CW9EM 


MIL-A- 

3669 


35 


n- 

CONTACT 

1001*83 


SEE NOTE 15 

34 

81 

61 

INSULATION SLEEVING ,ELEC 

1006776 - >S 



33 

ft 

6 

CLAMP. TORQUE MOTOR 

1000067 



32 

2 

2 

SCR, BUT. HO, SELF LKG, SPL. SOC 

IOOOZ50 -Z 



31 

6 

6 

SCR.CAR SELF LKG. HEXHD-SOC 

WW352CC2U4 



30 

1 

1 

RING FOAM 

,001515-1 



29 

6 j 

~6~1 

SCR. BUT HO. SELF LK6.SPL SOC 

10002*3-15 



26 

6 

in 

SCR. CAP, SELF LKG. HEX HD,SOC 

iAsasy^4a4 



27 

4 

3: 

SCR, FLAT HD. SELF LKG.HEX.SOC 

lOOOir 4-17 



26 

4 

4 

WASHER. FLAT. ROUNO 

iooor’54 



25 

7 

7 

SCR. BUT.HD. SELF LKG, SPL SOC 

I000£50-I2 



24 

6 

6 

SCR. BUT. HD. SELF LKG. HEA.SOC 

IOOOC 93-25 



23 

6 

6 

SCR. CAP. SOC HO, HEX 

IOOOIIO-T 



22 - 

A/R 

a/r 

SOLDER 

SN6C WARP 2 

IQC- S 

-57/ 


21 £ 

A/R 

A/R 

SOLDER 

SN IJ WARP 2 

QCS 

-57| 


20 - 

2 

2 

NSULATION SLEEVING .ELEC 

1006776- 9 


.3k*— 

J3- c 

2 

2 

BUSHING, INSULATEO 

ICC0036 



16 

6 

6 

TERMINAL. INSULATED 

ICCOlOO-2 



17 

ft 

ft 

TERMINAL. INSULATED 

»coioo-r 



« ‘ 

1 

1 

CUP. RETAINING 

UC_'?8 


15 < 

2 

2 

CONNECTOR,ELEC. RECP 29C0NT I000H6 

j 

14 1 

2 

2 

CONNFCTOR. ELEC. PUJG 29 CONT 1600117 

; 

a 

2 

2 

BRACKET, CONNECTOR 

1000125 


a - 

1 

1 

A'/Y, RING, FRICTiON 

‘ 1C w ' ' 16 


ii 

1 

1 

RETAINER, BEARING I.A.4 M.A. 

1001481 


10 

1 

1 

BEARING, BALL. DUPLEX, j w 

• CCI483 




"o 

! 

’ _l_ 

GUIDE. WIRE. STUB SHAFT M.A 

1000152 




e 

1 

’ 1 

GUIDE, WIRE, BR&HS& M.A. 

,000092 




7 

1 

1 

MOTOR. TORQUE. OC.FRAMLESS 

1000075 j 

6 

1 


Rt-A : NER, R \G, - R C T ON 

'CO - 3 I « 

5 

1 

__r 

R5VR ASSY, IX X**TR t PITCH-YAW 

1000030 ! 5 ~ 

4 

1 

i 

SLIP RING ASSY. ELEC.40 Con 

1000037 ) 

3 

1 

_ —— 

SHAFT. STUB. 1X MIDOlE AX S 

ICO-4 8 2 


{ j“ 

~ ~T 

HOUSING, BEARING, 1X INNER AX £ 

IOOO cc 

J_!_ 

i 

El 

!pj 

NOMCMCLATUMf 

OH MSCIHPTIOM 

MAT 0« 

lOCMTirviNG MO 


‘KAMO* 

MATtMAl 

W HOTM 

’MO 

HO 

■RT r 

REQ' 

□1 list or carts and materials 1 

--—-1 .- - .- »- BIT 1 "1 


QQ 


00 wot KALI 1HM 0 



NTER GIMBAL 
SUB-ASSEMBLY 

ONE SPEED MIDDLE AXIS 


$MCtcfc>rr cfwifo 


100150Q 


wt • I_t ‘ I 


0 





































































































































MMMJM <UCTWI IQHU I 

/66EMBLE (TEST PER THE REQUREMBffS OF AfTP IOOISOB 
USE CMCAfiO STITCH UCM& M AREAS NKXTO. 

LEAK MUST NOT EXTEND «M TMI MOUE. 

USE FltuRE ElSMT STiTCH LMCtNS IM AMKI IMMCATSD 


, SELECT ITEM (3A) TO MEET TORQUE RtQJlMMEhTS CF R TF lO OPOOS 
JG.WEAT SHRINK SLEEVING, ITEM Cip.TO ITEMS ® $ ® AFTER ASSEMBLY 

















































































































6 


WIRING LEGEND 


to BC* not* I* 




SECTION C-C 

e places 



DETAIL E 

SCALE 4/1 

IOOI 510 -I 


* \© 


SEC NOTE 4 



£-1562 RAO MAX 
SGE NOIE IS 


SEE NOTE S 
-t PLACES 



SHOWN WITH ITEM’S 
® REMOV© 


L INT ER PR E T ORMMMG IN ACCORDANCE WITH ML-0-70St7 •» 

2. mark characters WWW COLOR VLPCIL PER ND 100201* AT 

LOCATION SHOWN. IA 

S. ECCE NTRICIT Y MARKS ON BOTH RACES Of ®TO BE ALIGHCO WITHIN It 

VOfFcBaho in the direction or the arrow shown WHEN It. 

(V)f CD are m position shown, apply thin coat or (So) to insoe is 

DIAMETER 0T(js)AND TO FAYWG SORfACC OF(J[)3Cro*t ASSEMBLY 14 

4. APPLY (|T) ON THE THREADS OF (T) OR (4?) BEFORE ASSEMBLING 
* IDENUFT USING 0W6. NO. .REVISION LETTER, MANUTACTUERS SYMBOL FSEFIAL NO. QL 
ONQj< MATCHING SERIAL NO. ON® AT ** INDICATED LOCATION TER NOTE. I ^ 

& SCREW TORQUE REQUIREMENTS 1 7* 

CO© 40 Bkt* 

@ IOIN-L* 

©CD®® 5 IN-LB 

(35® S5IN-LB 

T SOLDER ALL LEADS FR0M(T)<® TO LOWER SECTION OF APPROPRIATE 
TERMINAL PER MIL-STD-440 USING ® SOLDER ALL OTHER LEADS TO 
Either upper section or appropriate ternwnja. pgr ml-std-440 

USING (a): WIRE INSULATION SHALLK WITHAL 46 OP SOLDERED CONNECTIONS. 



■ SEC NOTE t 
TYP 


SHOWN WITH 
(J5) REMOVED 





dD— 

l PLACES 


CAUTION: DO NOT SEPARATE STUB SHAFT FROM MSA. INC- fT^ OR AEAAOW TORQUE MONO® 
WITHOUT FIRST ASSEMBLING KEEPER TO TORQUE MOTOR® 

MAXIMUM ALLOWABLE TORQUE IB OAHH. 

ASSEMBLE AND TEST PER. THE RCQOUAMEMTS OF P*R ATP IOOOOIO 

USE OHCRQO ATTACH L A ONA IN ARM IUMCRTEO __ 

LEADS MUST NOT EXTEND BR.YOMO THIS RAMUS. ( ^ _ 

ALL SPARC LEADS TO BE S.OO 1 .It LONG f TO TERMINATE NEA ^ IA y AFTER TOUXNB 
BACK ON THEMSELVES.ENDS TO BE INSULATED BEFORE WRaPTOG INTO HARNESS 
USE FIGURE EIGHT STITCH LAONG M AREA INDCMED 

ICAT SHRWK SLEEVING ON ITEMS ©T® AFTER ASSE TWISTING 10 CONSIST 0FTI« 
FOLLOWING NO OF TURNS PER INCH 


SHOAAI WITW(S) REMOLD 


IOOI5IO-2 


MOl OF LEADS 

2 OP 5 _ 

"TTOR MORE 


L TURNS mm I MDI 



1001510 1 AI 


6 




















































































































































































.LA .001 
— B — 



)20 ajL, 

“TT 


-.62S-32N5-2A 
LENGTH OF ENGAGEMENT .2IS 

MAJOR DIA ?79 
PITCH 0»A : *°l% - 
MINOR OIA .5856 NOMINAL 
PD# A.005 TIR T_ 

PD1B .002 _: z 


.020 y jc* tit*. 

.040 X 45 “ 5 


RELIEVE TO ROOT DIA- 
OF THREAD , 



. .010 « iri.e* 

.020 X XS 


.729 0IA 


-:8fl SL0T 


SEE NOTE 4 


‘ 500 *IA I " A ~ i 

.501 I 

I#A .0005 T!R| ” 


J .1880 

.225 L 

.22.Q 


.005 R MAX 




SECTION A-A 


NOTES _ 

J. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED 
BY MIL-D-70327 

2. £ ^/ FINISH UNLESS OTHERWISE SPECIFIED 

3. BREAK ALL SHARP EDGES *gf| — 

4 IDENTIFY USING DRAWING* NO., REVISION LETTER AND MANUFACTURERS 
SYMBOL AT INDICATED LOCATION PER NDI002OI9 
5. INSIDE CORNERS .010 R MAX UNLESS OTHERWISE SPECIFIED 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHM 
TOLERANCES ON 


MIT 

INSTRUMENTATION LAB 

CAMSKIOOC. MAM. 


FRACTIONS DECIMALS ANGLES CHECKED - 

^ ± - A — Apponyn) > 

DO NOT SCALE THIS DR AWING 

_ MATERIAL TITANIUM ***<*&> 

DL1001500 ALLOY BAR, 6AL-4V APPROVED i 

-CLASS 5, PEA — “ ,T J 

- MIL-T-9047 APPROVES^ 

L (CATION MSc”^ 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 

RETAINER, 
RIN$ FRICTION 


II COOE CENT NO.I SIZE I 


1001513 






















“ I?JOIA THRU 

iei«&fs?5as6si 

l CSINK 05*-5* TO ||g OIA 
\ 3 HOLES SPACED AS SHOWN 
\ON 4.125 DIA BSC 1^ B OIO PI A 


-NO 2 «)86}56 NC-2B 200 MIN FULL THO 
CSK S^tS* TO j§ DIA 2 HOLES 
SPACED AS SH OWN ON 750 DIA BSC 
to A004DiAl 


r NQ4(ll2)40NC-2B 
250 MIN PULL THD 
CSK 85**5*T0 jggDlA 
6 HOLES SPACED AS 
ON 4.125 DIA BSC 


lifD'Agl DEEP— 
'3 places eoually 
SPACED ON 4.125 
DIA BSC 
K&E .010 DtA~l 


DATUM PLANE J 
II G .0002 
SEE NOTE 8 



\l% DIA THRU- 

250 DIA CBORE 625 DEEP 
6 HOLES SPACED A S SHQ 
ON 4125 OIA BSC[4>0 QC 


SEE DETAIL G 





r-3l2 TYP h-D 


4|?wide slot 

6 PLACES EQUALLY SPA 
ON A 4.375 OlA BSC g 

2SQ 4 MII? FULL 0 THD 
CSK 85*15* TO \l DIA 
6 PLACES EQUALLY SR 
ON A 4.312 DIA BSCR 


SECTION A-A 


“238OIA THRU 
Si2DiA CBORE 
SF -390 DM TO C 
CSK 60ri5*T0 


•SHOMM-FNttK— 
DIA— FARSlOE — 


‘-NO 4(112)40 NC-28 THRU 
CSK 05*-5*TO || DIA 
3 HOLES EQUALLY S PACED 
SEE SECTION A"A l^BOOSOIAl 


4.312 n rr 

^4,302 01 A 

9 D piotirI 


DETAIL G 

4 PLACES EQUALLY SPACED 
WITHIN L005 
SCALE 2/1 


- .625-32 NS-2 B 
LENGTH OF ENGAGEMENT .218 
MAJOR DIA .625 NOMINAL 
PITCH DIA ;|gg 


fp3#A.00fe TIR 
IPU-L F .002 


818 R all edges 

OF SLOT 


■HL_— 

SEJTON B-B 


SECTION C-C 

SCALE 2/1 
2 PLACES 


•010 y f K 
.020 x 452:5 
2 PLACES 


INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 
2^MACHME FIMSH UNLESS OTHERWISE SPECIFIED 
3BHEAK SHARP EDGES g?§ 

4IN5I0E CORNERS DIO RAO UNLESS OTHERWISE SPECIFIED 

^InuSctVIers's^mbS.’S mS&FQSRtiST 0 

PFR MIL-STD-130 

T ^ , y^SJ»t« TE 9 ,ff < aNTER * 

BUNE PASSING THRU CENTER OF SURFACE A $ CENTER OF 
SLOT H ESTABLISHES DATUM RTaNE J 


/ 

7 *^ 

.030 

nan 


R£g X 45* iS* CHAMFER 7 
ALL AROUNO / 



3500 OIA 
DATUM 


DETAIL E 


VIEW D~D 

scale 1 / 


XX45*155— 
CHAMFER 3|g 


838w,oe- 

x 828 deep 


-j 30 DIA THRU * 

CBORE .187 DIA TO DIM SHOWN 
CSINK 60* tr TO j|g OIA 
8 HOLES 

M38*45*15* CHAMFER 


SECTION F-F 

scale 2/1 


UST OF FARTS AND MATEIMAU 


™»»iHjTwr SHAFT, STUB __J 

SS ONE SPEED (DUTERAXS—- 


00/506 [Pl-i0oi3oo| 


BERYLLIUM 
BRUSH SPEC S-20Q 
ALT: SPEC ML- B-2151 







































































































V SISIOOI 


_ REVISIONS Tbgg \)2U 

DESCRIPTION I DATE 


ITDRR 147 86 


UOO u '“ 
SEE NOTE 
4 , 



115 Dec ^4 


APPROVAL 


957 °l A 

SEE NOTE 

4 



MOLDED SURFACES 


NOTES 

I. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-T032T 
MATERIAL*. POLYURETHANE FOAM tV THK PER MIL-P-265I4A(ASG) 

TYPE I, CLASS 2, (MOLDED) DENSITY OF FREE BLOWN FOAM 2.0/3.0 LBS/CU. FT. OPEN CELL 
— 3. IDENTIFY USING DRAWING NO., REVISION LETTER, CURING DATE AND 
MANUFACTURERS SYMBOL PER ND10020I9 

4. THESE SURFACES MAYBE PUNCHED,CUT,OR MACHINED 

5. THE AVERAGE PART DENSITY SHALL NOT EXCEED 6.0 LBS./CU.FT. 


I00IEI0 

1001508 

1001506 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


M I T 

INSTRUMENTATION LAS 

CONTRACT 


__ DO NOT SCA LE THIS DRAWING 

)6 DL1001500 MATERIAL; 

tSY USED0N SEE NOTE 2 

APPLICATION 




LIST OF PARTS AND MATERIALS 


RING, 

FOAM 


CODE I DENT. 


MIT 

INSTRUM ENTATION 
LABORATORY 

Cambridge. Mass. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001515 

















NOTES 

ZI l. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-7033T 

— a. MATERIAL: POLYURETHANE FOAM 1^ THK PER MIL-P-E65I4A(ASG) 

— TYPE r, CLASS 2, (MOLDED) . DENSITY 3.0-10.0 LBS/CU.FT, OPEN _CELI_ 

_ 3. IDENTIFY USING DRAWING NO., REVISION LETTER, AND __ 

.77 MANUFACTURERS SYMBOL PER NDI002019 . _ _ 7 . 


QTY. 

NOMENCLATURE 

PART OR 

SPECIFICATION 

MATERIAL 

FIND 

REQD. 

OR DESCRIPTION 

IDENTIFYING NO. 

OR NOTES 

NO. 


LIST OF PARTS AND MATERIALS 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 



FRACTIONS DECIMALS ANGUS 

10 01ET10 


- - - 

1001508 


DO NOT SCALE THIS DRAWING 

1001506 

DLIQQI500 

MATERIAL: 

NEXT ASSY 

USED ON 

SEEL-NOTE 2 


M I T 

INSTRUMENTATION LAB 
CONTRACT 


NAS 9-15: 



m 


DRAWN IE 


ISC 




.yd^ction^TT , 


"RING, 

FOAM 


SCALE 

2/1 


UNIT WT. I CODE IDENT. 


■ ' ft t f ... 

INSTRUM ENTATION 
LABORATORY 
Cambridoi. Maw. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001515 


SHEET .11 OF_1 


APPLICATION 






























IfCCIPICATKMM. M OTHK* DATA 
fSF.SH®.!?* AMV OTHKH THAN IN COHHKCTION WITH A DKFIHITKLV 

S*°* 1 *" 1 " T ^"OCUAfNCNT OPCRATION. THK UHITKO STATU COVKRN* 
•* K:UB » "O RKSPOKSIMLITY NOR ANY OBLIGATION WHATSOIVIR: 

r-.J?* ™* T ™ B •OTMHHSNT may navi pormulatio. purnishio. or 

{* *"* SMPPt-ltO THK SAID DRAWINRS. SPSCIPICATIONS OR OTNKR DATA W 

!*g L.T?..P « RKRAROCD RY IMPLICATION OR OTHER Will AS IN ANY MANNER 
LJCKWSINR TNE HOLDER OR ANY OTNKR PKRSON OR CORPORATION. OR COMVKY- 
“***"/- °* *«»■»—*>«» TO MANUPACTURK. USK. OR HU AMT 

PATENTS* INVENTION THAT MAT IM ANY WAY DC RELATED THERETO. 


REVISIONS TDRR 1)21 


.030 MAX- 
2 PLACES. 


.040 MAX 
2. PLACES 


2) Ref 


COMPLETELY FILL C 
: BETWEEN ITEM(] 

WITH ITEM (IT) 


arakit: 


DETAIL z 
SCALE 4-1 


SEE DETAIL 




1*101 i}| A 

J.IOO D1A 
)A.005 TIRl 


CONSTRAINED 
... SEE NOTE 3b 


SEE NOTE 3d 


SECTION A "A 


notes:': .... _ ___ 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-7032T . .— 

2. IDENTIFY USING DRAWING NO., REVISION LETTER AND 
MANUFACTURERS SYMBOL PER NDI002.0I9 1 

3. ORDER OF OPERATIONS (PROCESS MANDATORY) __ __ 

TZL a. BOND PER ND 1002004 TYPE TX SEMI-RIGID ( MAX CURE TEMP 200«f) 

~ USING ITEM(j[)(sEE DETAIL E) _ _ 

_T b. FINISH MACHINE ‘ ,l °J/|.loo VIA WITH ASSEMBLY LN CONSTRAINED CONDITION,.:. VT ll 
CONSTRAIN OR CLOSE RING GAP BY USING A THIN FLEXIBLE BAND ABOUT THE OUTER RING 
CIRCUMFERENCE AND APPLYING A FORCE AT THE ENDS OF THIS BAND, TANGENT TO THE RING. 
JIG TO MAINTAIN THIS RING SHAPE BEFORE REMOVING BAND FOR MACHINING 


A/R 1010 684 
A/R IOIOCST 
I 1001517 

I 1001518 


CATALYST 

EPOXY RESIN (CLEAR) 

RING, WEARING _ 

RING, SPLIT, FRICTION 


10015 IO 

1001508- ~ 

1001506 DLI00I5OO 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES INSTT 

CAPACITOR VALUES ARE IN < 

RESISTOR VALUES ARE IN OHMS - 

TOLERANCES ON DRAWN _ 

FRACTIONS DECIMALS ANGLES CHECKED 

DO NOT SCALE THIS DRAWING APPROVE! 


APPROVED 
MIT _ 


PART OR 
IDENTIFYING NO. 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


MATERIAL 
OR NOTES 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 




MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 

: ASSEMBLY, 
RING, FRICTION 


CODE IDENT NO. SIZE 


DRAWING NO. 


1001516 


APPLICATION 


3 


1 























8 


7 


6 


5 



4 


3 


2 


1 


S- 


REVISIONS TX>RR II Z\Co 


SVM 

ZONE 

DESCRIPTION 

OR 

CHK 

OATS 

APRR 

OVED 

A 


REVISED PER TDRR 

— ■ 



4 /< 

d 


f 


!of8 d ‘ a th * u on ‘.its mA 

2 HOLES 


5 


.004 

.006 


2 PLACES 


2 PLACES 



SECTION A "A 


il 


CONSTRAINED 

SEE NOTE 5 


\ 














1001516 

D LI 001500 

NEXT ASSY 

USED ON 

| APPLICATION | 




PART OR 

MATERIAL. 

NOMENCLATURE OR 

E3 

IDENTIFYING NO. 

OR NOTES 

DESCRIPTION 

ESI 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
CAPACITOR VALUES ARE IN 
RESISTOR VALUES ARE IN OHMS 
TOLERANCES ON 

ANGLES) 


DO NOT SCALE THIS DRAWING 


MATERIAL CRES 440 C 

PER SPECQQ-S-762 
COND A FORM BAR 
FIH HOT OR COLD _ 


MIT 

INSTRUMENTATION LAB 

CAMBRIDGE. MASS. 


drawn 




UST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


RING, SPLIT 
FRICTION 


APPROVED 
MIT 


’J4 


mmm\ 


CODE IOENT NO. 


dateH scale a /T 


DRAWING NO. 

1001518 

| SHEET | <?TT" 




















£00 LB * TENSION to diameter 



NOTES 

L INTERPRET DRAWING IN ACCORDANCE WITH MIL-0-70327 

2. 6 \/ FINISH UNLESS OTHERWISE SPECIFIED 

3. INSIDE CORNERS .010 R MAX 

4. REMOVE BURRS AND BREAK SHARP EDGES 

5. RING MUST BE FINISH MACHINED IN CONSTRAINED CONDITION. CONSTRAIN OR CLOSE GAP 

_ OF ROUGH MACHINED RING BY USING A THIN FLEXIBLE STEEL BAND ABOUT THE OUTER RING CIRCUMFERENCE 

AND APPLYING A FORCE AT THE ENDS OF THIS BAND TANGENT TO THE RING. 4IG TO MAINTAIN THIS RING 
SHAPE BEFORE REMOVING BAND FOR MACHINING 
4. ORDER OF OPERATIONS J (MANDATORY) 

A. ROUGH MACHINE 

I B. HARDEN TO R C 5^-60 PER MIL-H-4875 

C. FINISH GRIND 

D. PASSIVATE PER MIL-F-14072 FINE 300 

T IDENTIFY USING DRAWING NO ., REVISION LETTER AND MANUFACTURERS 
I SYMBOL PER NDI002019 


/ 

\ 


4 


3 


2 


1 



REVISIONS TDRR \\Z\Q> 


-:§f8 D,A THRU ON its OIA 

2 HOLES 



SECTION A "A 


CONSTRAINED 

SEE NOTE 5 



















notes: 

I. INTERPRET DWG IN ACCORDANCE WITH MIL-D-70327 

2. MAT'L: URETHANE FOAM PER MIL-P-26514 A TYPE I.CLASS 2; CELL STRUCTURE, 
OPEN CELL*.COLOR,BLACK;DENSITY OF PART 2.5 TO 3.0 LBS./CU.Ft..THERMAL 
CONDUCTIVITY AT 75°F - 0.30 BTU/HR. SQ.FT. fF/IN) MAX.;SURFACE TO KAYE 
WATER-SHEDOING CHARACTERISTIC.MAT'L SHALL NOT SUPPORT COMBUSTION AND 
SHALL BE SUITABLE FOR SERVICE AT A MAX TEMP OF 200° F. 


3.1/32 MAX RADIUS UNLESS OTHERWISE SPECIFIED 

4 . WALL THICKNESS TO BE 1/4+^ 16 

5 . IDENTIFY USING DWG. NO.,REV.LETTER 8 MANUFACTURERS SYMBOL PER ND1002019 


3 


2 



1 


Si «•%:. 


















Liffl 


jgywssTsajss; 

l CSINK 0 b*t5* TO j|8 DIA 
\ 3 HOLES SPACED AS S H QWN 
\ON 4.125 DIA BSC |^ B 010DIA 


-NO 2 4)06)56 NC-2B 200 MIN FULL THO 
CSK §5*;S’ TO DIA 2 HOLES 


SPACED AS SHOWN ON 750 DIA BSC 
A004D!a1 


r-NQ4 (ll 2) 40NC-2B 
250 MIN FULL THD 
CSK 85*^5* TO j |8 DIA 

WSiSSStfatH 


DEEP- 

3 PLACES equally 


SPACED ON 4.125 
DiA BSC 
reE.oiooiAl 



17^30' / 

BSC X _ 

1 7*30BSC 


DATUM PLANE J 
II G .0002 
SEE NOTE 8 


•]£? DIA THRU-^"* 

250 DIA CBORE 625 DEEP 
6 HOLES SPACED AS SHOWN , 
ON 4125-DIA BSC|&b q05DIA| 


SEE DETAIL 6 



10ATUM PLANEGlSEE NOTE 7 


^■312 TYP H“D 


H^WIOE SLOT 


“SSo^^llN^FULL 0 TH? 
CSK 85*i5* TO ;J| DIA 


6 PLACES EQUALLY SB 
ON A 4312 DIA BSCR 


-U§?k 

SECTION A-A 


-Sit DIA THRU 
312 DIA CBORE 
• SF -390 DM TO 0 
CSK 60* 15* TO 


'-NO 4 (112) 40 NC-20 THRU 
CSK 05‘i5*TO [| DIA 
3 HOLES EQUALLY S PACED 

3H0WN-FARM*- SEE SECTION A~A l^ B OOS DIA! 
OIA— FARSlOE — 


4.312 niA 
-4302 01A 

m d qiotirI 


DETAIL G 


4 PLACES EQUALLY SPACED 
WITHIN ±005 
SCALE 2/1 


INTERPRET DRAWING IN ACCORDANCE WITH MK.-D-70327 
2^MACHINE FINSH UNLESS OTHERWISE SHtOHfcD 
1BHEAK SHARP EDGES 

4INSI0E CORNERS .010 RAD UNLESS OTHERWISE SPECIFIED 
S IDENTIFY USING DRAWING NO. REVISION LETTER, ANQ 



?€25-32NS-2B 

LENGTH OF ENGAGEMENT .218 
MAJOR DIA .€2F NOMINAL 


r$40 R ALL EDGES 
\0F SLOT 


PO (ft A .005 TIR 
PDX F .002 


Hk— u 


SECTION B-B 

SCALE 2/\ 



SECTION C-C 


scale 2/1 

2 PLACES 


•:§i£ WIDE R ;g£g DEEP 


DETAIL E 


40 X 45* ±5* CHAMFER 7 
ALL AROUNO / 


3.500 OIA 
DATUM 



PER ND 1002019 

< CB " 1 " y 

gSft A * *” * 

8* DENOTES ALL DIMENSIONS REQUIRED FOR REWORK OF 
ALL OTHER •MAENSIONS ARE REFERENCE 


SCALE 4/1 ~ 
SEE N QTE 9_ 


VIEW D'D 

SCALE 1/ 


8^X45* ±5*-- 

W CHAMFER 


040WIDE— 

Xg^DEEP 


“138 01A THRU ’ 

CBORE .187 OIA TO DIM SHOWN 
CSINK 60* ±T TO ||g OIA 
8 HOLES 


TYP 2 PLACES 


-g|8 X 45* t5* CHAMFER 


SECTION F-F 

SCALE 2/l 


LOT or PftWTS AWD MATEMAIJ 


SHAFT, STUB _ 
ONE SPEED OUTER AXE — 
(MOO) _ 


( 0OI50F DLI00I50C m m mm . I A) 

SnSl - h— m~ MAKE FROM NASA 

- ■—‘a " ■ DWG IOOOC "6 • ITT 


IOOI52Q 





























rj^jDIA THRU 
\ CSlNK arts* TO l|8 DIA 

\ 3 holes spaced as shown 

\ ON A 4.125 OI A BSC 
\|»BOIOD<A| 


SfrTXA SLOT 


t-No4(Jl2) 40 NC-2B 


j|f OIA 85 DEEP—. 
3 ft-ACES EQUALLY 
SPACED ON A 4.125 
DIA bX 

£ -QIQ Diin 


r-NO4 0t2)4ONC-2B 
250 MIN FULL THD 
CSK 85*15* TO jJgDIA 
6 HOLES SPACED AS SHOWN 
ON 4.125 DIA BSC 
I4B E Q05 Qia1 


DATUM PLANE J 
11 G 0002 
S&E NOtE * 


iraor 

bsc 45 050 

1 7-30'bscl!:/ „ i 

- 1 — 


18x45*15* CHAMFER 
*°BOTH ENOS 
A.QQ05TIRI 


> y\^-No 2 (086)56 NC-20 
' -280 MIN FULL THD 

?X250 CSK 85*15* TO JggDlA 

\ TYP 2 HOLES SPACED AS SHOWN_ 

\ ON 750 DIA BSC l& A 004 DIA 

k 45*0* - 

<2 PLACES ^SLOT F 


■& a w f?@» 


18?°“ 1 


SLOT F 

H-D 


A*/ '-SEE OETAIL 6 


IATUM plane 5| see NOTE 7 

--H-D 


If! DIA THR 
250 OIA CJS 


>0 DEEP 
AS SHOWN 


Lfl20 RAO MAX 


a 


cm 


-No 4(112) 40 N02B THRU 
CSK 85*15* TO ||8 DIA 
3 HOLES EQUALLY SPACED 
SEE SECTION F-FI# B 005 OIA 1 


-8J8" 


&T ’ <*? 

lie 00021 33 


-.238 OIA THRU 
312 DIA C80RE AS SHOWN 
ON 1450 RAO occ 
60* U* CSK TO DIA—FARSIDE— 


\ .187 DIA CBORE , 
YfVtrCSK TO jj 

\4 HOLES AS 


DIM. SHOWN 
DIA —FARSlDE- 


SECTION A-A 


-.625-32 NS-2B 
LENGTH OF ENGAGEMENT .21ft 
MAJOR DIA .625 NOMINAL 


BIIOR OUT J - TO DEPTH SHOWN 


1 U,A .591 2 
I A .005 TIR 
» F.OQZ 



SECTION B-B 

SCALE: 2/1 


-.QIQ y »r** r 
- .020 X45 15 
. 7 2 .PLACES ~ 


♦MS T** 

^-.040 WIDE X -.gig DEEP * 


1500 R TYr 
BSC 


88 ^ 

2 PLANS' 


hfOTES 

IftfERPRET 0RAWM6 IN ACCORDANCE WITH MIL-0-70327 
I^MACHNC FftftSH UNLESS OTHERWISE SPECIFIED 
fc BREAK SHARP EOGES 

A INSIDE CORNERS OIO.R UNLESS OTHERWISE SPECIFIED 


DETAIL E 


PER MD 100201 9 

w A< C£WB,0F 



R ALL EOGES OF SLOT 


._ SCALE 4/1 
SEE NOTE ft 


8f8* 45*15*- 
CUAMFER 


8i2x45*i5*-> 

CHAMFER 


jggx 45* IS* CHAMFER 
-858 WIDE xg^goEE*" 


3.-4 DENOTES ALL DIMENSIONS REQUIRED FOR REWORK QF 
ALL OTHER GMKNtlQNS ARE REFERENCE -— ~ — 


SECTION. C-C 

SCALE. 2/1 
2 PLACES 


H i# 0 QIOfiRl 


rgjgx 45* 15* CHAMFER j 
I ALL AROUND / 


DETAIL G 

4 PLACES EQUALLY SPACED 
W.THIN *005 
SCALE 2/1 


SECTION F-F 

SCALE: 2/1 


LIST OF MATS AND MATERIALS 


VIEW D-D 

SCALE: t/t 


shaft; stub 

ONE SPEED 
MIDDLE AXIS (MO®) 


[ ■ >00^0? pLjg gB SSS FROM NASA % 
I — 4 - — DWG 10001QE TTj 



3 ** 
























3 


Hftou T «RU 

\250 OlA CBOHE 437 DEEP 
\ NO 6 (138) 32 NC-2B THRU 
\CSINK 85*t5* TO !|8 DIA 
\ 3 HOLES SFPCED AS SHOKVN 
\ ON A 4,125 DI A BSC 


rll? °*A MILLED SLOT 
\ 6 PLACES EQUALLY SRA* 
\ ONI 4.375 OA BSC j^Tpl 

VNo40l2)4O NC-2B 

\ 2 c?teV H ;| 8! 



jlloiA^OEEP— 

3 PLACES EOUALIY 
SPACED ON A 
4.125 DIA BSC 
[&E.OIODIA] 


DATUM PLANE J 
II G .0002 
SEE NOTE 8 


ff DIA THRU- 



r-NO. 4 01 ^ 40 NC-2B 
250 MIN C ULL THO 
CSK 85*15*TO j|8 DlA 
6 HOLES SPACED AS SHOWN 
ON 4.125 DIA BSC 
I&EQ05DIA1 


> A 0002TIR 
— D — 

32/ 




,-£28 X 45*15* CHAMFER 
r ^ ' BOTH ENDS 


l see detail 6 


_L C POQI j 





-No 2 0086)56 NC-2B 
280 MIN FULL THD 
CSK 85*15* TO JggDlA 
2 HOLES SPACED AS SHOWN , 
ON .750 DIA BSC l& A 004 DIAl 


IDATUM PLANEGI SEE NOTE 7 

K-D 


i A Q002TIR 
—B— 


250 DIA CBORE 500 DEEP 




-Be8» TYP 


^020 RAD MAX 


312 DIA CBORE AS SHOWN 

ON 1.450 RAD. occ 

60*21* CSK TO DIA—FARSIDE— 


V J |38 D, A TMRU 

\.I37 DIA CBORE TO DIM. SHOWN 
\BE* tr CSK TO j|? DIA —FARSIDE— 

\ 8 HOLES ASSHOWN 


SECTION A-A 


\T® 


ri 


-.625-12 NS-2 B 
LENGTH OF ENGAGEMENT .EIB 
MAJOR DIA .625 NOMINAL 

PITCH DIA *i§3? — 


PD# A.005 TIR 
. P D3—FA302 



SECTION B-B 

SCALE: 2/1 


•OlO W 4|*4| 

^Q2Q i4S * ' 
_£ PLACES 


-.040*“ :, .OM 0reP * 


JfQISS. 

L INTERPRET DRAWING IN ACCORDANCE WITH MIL- D 70327 
2 6 ^ MACHINE FINISH UNLESS OTHERWISE SPECIFIED 
a BREAK SHARP EDGES 

4 INSIDE CORNERS .010 R UNLESS OTHERWISE SPECIFIED 

5 


®40 R ALL EDGES OF SLOT 


j '*A"ui5fORN? I SaRT”'TEMPERATURE"’of 68*F il*F . 

7 TOaB3U£^pS^ a < center of 

•$8r^*£g&mX£S5Fj A < CENTER * 

.%* DENOTES ALL DIMENSIONS REQUIRED FOR REWORK OF 
; ALL OTHER DIMENSIONS ARE REFERENCE 


: WITHIN SPECIFIED LIMITS AT 



DETAIL E 

T" SCALE 4/1 
_Z : SEE NOTE 8 


SECTION C-C 

SCALE 2/ 

2 PLACES 


. A.3I c. 

L ^43q; 

Hnroi 


g$X45*iS*-^ HI 


joIB x 45 ‘ ^chamfer 


WIDE DEEP 


r^iXX 45* 15* CHAMFER -j 
I ALL AROUND / 


DETAIL G 

4 PLACES EQUALLY SPACED 
WITHIU !0C5 
SCALE 2/1 


SECTION F-F 

SCALE. 2/l 


VIEW D-D 

SCALE: l/l 


UST or PARTS AND MATERIALS 


SHAFT STUB 

ONE SPEED 
INNER AXIS (MOO) 


I MAKE. FROM NASA 
DWG 1000057 


1001522 


5 



























































UNLESS OTHERWISE SPECIFIED 
I..— — DIMENSIONS ARE IN INCHES INSTRU 

CAPACITOR VALUES ARE IN pf CAI 

RESISTOR VALUES ARE M OHMS . ; 

_______ TOLERANCES ON DRAWN f— 

FRACTIONS DECIMALS ANGLES CHECKED _ 

A — 3k ““ 3k 1 "■ APPROVED^ 
___________ DO NOT SCALE THIS DRAWING * 

_ MATERIAL TITANIUM WW ” 8 

DLI00I500 ALLOY BAR* SAL^JEtf APPROVED J 

- ||Mn ■ — CLASS E,.PER_ M,T ” 

-MIL- T- 9041- approved^ 


MIT 

INSTRUMENTATION LAB 

CAMBRIOOC. MAS*. 


MANNED SPACECRAFT CENTER 

HOUCTON, TOA*_ 

RETAINER, RING, 
FRICTION (MOD) 


ICOOE IOCNT NO.I SIZE I 


DATE I SC** 4/1 


1001524 



























































































REVISIONS _ pyCUl 

ZONE SYM DESCRIPTION | DATE APPROVAL 

_: A #£V/S£OA£# 7~£>tt OS3tO tl/ufo (jU 


INTERCONNECTIONS 
LI-I (SEE NOTE 2)1 L2-T~ 
LI-3(SEE NOTE 2) L2-3 
LI-9(SEE NOTE 2) L2-9 

LI-6 _ L2-6 

LI-8 L2-8~ 

LI-II I L2—iT 

L2-7(SEE NOTE 2) L2-I2 


LEAD IDENTIFICATION 
ON SCHEMATIC I ON REACTOR 


GREEN (L2) 


.50 DIA 
MAX 


SEE NOTE 


RED (LI) 


14 PLACES 


;88 MAX—H 6.00 MIN 
14 PLACES 


MIN L— 


Ll-I 

LI-2 

LI-3 

LI-4 

LI-5 

LI-7 

LI-9 

LI-10 

LI-12 

L2-2 

L2-4 

L2-5 

L2-7 

L2-I0 


RED I 
RED 2 
RED 3 
RED 4 
RED 5 
RED 7 
RED 9 
RED 10 
RED 12 
GRN 2 
GRN 4 
GRN 5 
GRN 7 
GRN 10 


WINDING RES I STANCE (REF) 
±20%<®25°C 


FROM 

TO 

OH IV 

Ll-I 

LI-2 

10 

LI* 3 

LI-4 

10 

Ll-I 

L2-2 

10 

LI-3 

L2-4 

10 

LI-5 

L2-5 

190 

LI-7 

L2-7 

180 

LI-9 

LI-10 

25 

LI-9 

L2-I0 

25 

LI-12 

L2-7 

15 


notes: 

1. INSULATE BETWEEN REACTORS WITH .002 MYLAR TAPE PER MIL-I-15126. 

2. BRING OUT ONE LEADWIRE. 

3. PREHEAT WINDING AND IMPREGNANT TO 250°F. IMPREGNATE WINDING WITH IMPREGNANT. 
PULL NO VACUUM. BAKE 24HRS AT I80°F 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. SET LEADS EQUALLY SPACED AROUND PERIPHERY OF 

WINDING, WITH MYLAR TAPE PER MIL-I* 15126, ORDER OPTIONAL 

6. PART NO. 1001529 MUST BE A MATCHED PAIR. 

7. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 
. I 10MEGOHMS WHEN MEASURED AT 250VDC AFTER BAKING 

8. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED 
BY MIL-D- 70327 


A/R WIRE (LEADS) 
A/R IMPREGNANT 

A/R TAPE _ 

2 CORE 8 COIL ASSY 


NOMENCLATURE 
OR DESCRIPTION 


1 006711-13 
1010687* 1 

1001529 

PART OR 
IDENTIFYING NO. 


AW6 30 


SPECIFICATION 


SEE NOTE 5 
SEE MOTES 314 
SEE NOTE 1 ' 
SEE NOTE 6 " 

MATERIAL 
OR NOTES 


__ 1000285 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS OECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL 


M I T 

INSTRUMENTATION LAN 

COMTRACT 


1/€W _ 

for MSC 


LIST OF PARTS AND MATERIALS 


REACTOR ASSEMBLY 

(FIRST STAGE) 


SCALE 

NONE 


CODE IDENT. 


INSTRUM ENTATION 
LABORATORY 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001528 

T | OF | 



I Z « 

photographk?scale only j 






















1 


I 


[ INTERCONNECTIONS ' | 

li-ksee NOTE 2) 

L2-I 

LI-3(SEE NOTE 2) 

L2-3 

LI-91SEE NOTE 2) 

L2-9 

LI-6 

L2-6 

LI-8 

L2-8 

Ll-ll 

L2-II 

L2-7(SEE NOTE 2) 

L2-I2 


[ LEAD IDENTIFICATION | 

ON SCHEMATIC 

ON REACTOR 

Ll-I 

RED 1 

LI-2 

RED 2 

LI-3 

RED 3 

LI-4 

RED 4 

LI-5 

RED 5 

LI-7 

RED 7 

LI-9 

RED 9 

LI-10 

RED 10 

LI-12 

RED 12 

L2-2 

GRN 2 

L2-4 

GRN 4 

L2-5 

GRN 5 

L2-7 

GRN 7 

L2-I0 

GRN 10 


0 


GREEN (L2) 



ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 


A 

&£l//S£0 7~0PP OS3S0 

tt/ufr 3 

vA. 


3 

REVISED PE# TVRR U6& 

Mi 



RED (LI) 


SEE NOTE l(2) 



14 PLACES 


A. 


-.88 MAX- 


6.00 MIN 
14 PLACES 


WINDING RESISTANCE(REF) 

± 20%'<® 25°C 

FROM 

TO 

OHMS 

LI - 1 

LI-2 

10 

LI' 3 

LI-4 

10 

LI - 1 

L2-2 

10 

LI-3 

L2-4 

10 

LI-5' 

L2-5 

170 

LI-7 

L2-7 1 

180 

LI-9 

LI - 10 

25 

LI-9 

L2-I0 

25 

LI-12 

L2-7 

15 


notes: 

1. INSULATE BETWEEN REACTORS WITH .002 MYLAR TAPE PER MIL-1-15126. 

2. BRING OUT ONE LEADWIRE. 

3 PREHEAT WINDING AND IMPREGNANT TO 250°F. IMPREGNATE WINDING WITH IMPREGNANT. 
PULL NO VACUUM. BAKE 24HRS AT I80°F 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. SET LEADS EQUALLY SPACED AROUND PERIPHERY OF 
WINDING, WITH MYLAR TAPE PER MIL'I* 15126, ORDER OPTIONAL 

6. PART NO. 1001529 MUST BE A MATCHED PAIR. 

7. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 
10MEGOHMS WHEN MEASURED AT 250VDC AFTER BAKING 

8. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED 
BY MIL-D- 70327 


LIST OF PARTS AND MATERIALS 


M i T 

INSTRUMENTATION 
LABORATORY 
Cawwioo«. Ma—. 


M I T 

INSTRUMENTATION LAS 
CONTRACT 

NAS 

•PROVED 


/eve/ 


DATE 


f APPROVCO FOR MSC 

pj O 


REACTOR ASSEMBLY 

(FIRST STAGE) 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA OS AWING NO. 

1001528 


SHEET 


I Of | 










«.*«***-4 


ZONE SYM 


DATE I APPROVAL 


INTERCONNECTIONS 
LI-I (SEE NOTE 2) 1 L2-f~ 
LI-3(SEE NOTE 2) L2-3 
LI-9'SEE NOTE 2) L2-9 

LI-6 _ L2-6 

LI-8 L2-8 

Ll-ll _ L2-II 

L2-7CSEE NOTE 2) L2-I2 


LEAD IDENTIFICATION 
ON SCHEMATIC I ON REACTOR 


GREEN (L2)- 


.50 DIA 
MAX 


SEE NOTE l(2) 


RED (LI) 


14 PLACES 


188 MAX- 


( 6.00 MIN Y 
14 PLACES 


Ll-I 

LI-2 

LI-3 

LI-4 

LI-5 

LI-7 

LI-9 

LI-10 

LI-12 

L2-2 

L2-4 

L2-5 

L2-7 

L2-I0 


RED I 
RED 2 
RED 3 
RED 4 
RED 5 
RED 7 
RED 9 
RED 10 
RED 12 
GRN 2 
GRN 4 
GRN 5 
GRN 7 
GRN 10 


notes: 

1. INSULATE BETWEEN REACTORS WITH .002 MYLAR TAPE PER MIL-1-15126. 

2. BRING OUT ONE LEADWIRE. 

3. PREHEAT WINDING AND HYSOL TO 250°F. IMPREGNATE WINDING WITH HYSOL. 
PULL NO VACUM. BAKE 24 HRS AT I80°E 

4 . WIPE IMPREGNATION DURING CURE CYCLE. 

5. SET LEADS EQUALLY SPACED AROUND PERIPHERY OF 
WINDING, WITH MYLAR TAPE PER Mll-I-I5I26,0RDER OPTIONAL. 

6 . PART NO. 1001529 MUST BE A MATCHED PAIR. 

; 7 . Tfk RESISTANCE BETWEEN WiNd/NqS Si/aLL Nor BE LESS tNaN 
_ ... toMEGOt/MS H/NeN MEASt/RED AT SOOi/OC AFTE/% £AA?7j /<*— 




A/R WIRE(LEADS) 

A/R HYSOL _ 

A/R TAPE _ 

2 CORE ft COIL ASSY 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


1006711-13 

1Q1Q687-1 

1001529 

PART OR 
IOCNTIFYINQ NO. 


SPECIFICATION 


SEE MOTE 5 
SEX H0TES3I4 
SEE NOTE 1 " 
SEE NOTE 6 

MATERIAL 
OR NOTES 



UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MIT 

INSTRUMENTATION LAB 
CONTRACT 


I onAWH lyeVc/ 
APPHOVtO FOR MSC 


1000285 


LIST OF PARTS AND MATERIALS 


REACTOR ASSEMBLY 

(FIRST STAGE) 

SCALE I UNIT WT. I CODE IOENT. 


INSTRUMENTATION 
LABORATORY 
Cmwwiow. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001528 


APPLICATION 


3 





















































2 


TOTAL NUMBER WINDINGS 6 


TURNS AWG WIRE 
~ SIZE ^ 

TYPE OF 
WINDING 

160 41 

RANDOM 

160 

RANDOM 

800 

RANDOM 

COMMON 

800 : : 

RANDOM 

COMMON 

200 ‘ 

RANDOM 

COMMON 

50 

' r ..._ ^ 

RANDOM 

COMMON 


. : W1ND1hlG DATA 


.'WlMOIVlG : 
RESlSTAKlCI 

OHMS-20% 6)25Z{ 

K) 


lehg,th .size 

6 <3 


LEAD S _ 

I IDENTIFICATION 
£ START I FINISH 
I 2 




Noris: 

T- INSULATE BETWEEN WltlDlllGS tio.! 4 ll0,2 WITH A .005 POLYESTER WASHER 
rPEFt MIL-I-G3I TYPE G- 
' 2 - CORES MUST BE A MATCHED QUAD 

AND TWO PARTS 1001529 BE MADE. 4 ~ 

3- WIND WINDINGS OVER ENTIRE. LENGTH OF CORE. I-— 

4- TURNS OR TURNS RATIO TOLERANCE ±1%. 1 

5- («) DENOTES THE SAME INSTANTANEOUS POLARITY. | 

6. BEFORE WINDING* TEMPERATURE CYCLE CORES FOR A , 

MINIMUM OF 5 DAYS PER ND-1002209. CORES MUST MEET 1 

PERFORMANCE REQUIREMENTS OF SCO 1010688 AFTER I 

TEMPERATURE CYCLING. 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS I 

PRESCRIBED BY MIL-D-70327. 1 


.400.0 
•ZZ I.D. 


SEE KlOTE 5 


JORE I 


_ - _ REVISIONS _ Q3SU _ 

ZONE SYM DESCRIPTION DATE APPROVAL 

A REVISED PER TDRR Of 3* I ifa/n U>tf. 



SCHEMATIC 

"CuulJ 12 

9^WOG5JIO 

7^WDG4j8 

5 ^yDG3j 6 

V- v \ \ CORE 2 


.435 -p-4"! 

^ MAX I 


.480 OIA 
MAX 


r*rii 


A/R POLYESTER 
A/Z WIRE 
2 CORE 


Mj 


NOMENCLATURE 
OR DESCRIPTION 


1006711-22 

ioiofeea -1 

PART OR 
IDENTIFYING NO. 


AWG 41 


SPECIFICATION 


SEE tlOTE I 
SEE DATA 
SEE tlOTE Z 

MATERIAL 
OR NOTES 


1001528 

NEXT ASSY 


1000285 

USED ON 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGUS 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M I T 

INSTRUMENTATION LAS 
CONTRACT 


CHECKED £ 
PRAWN Jejj 
APPROVED FOR MSC 


APPLICATION 


LIST Of PARTS AND MATERIALS 

CORE 8 COIL 
ASSEMBLY 
(REACTOR 1ST STAGE 
MATCHED PAIR) 

SCALE UNIT WT. CODE IDENT 

NONE /- - 


INSTRUM ENT ATION 
LABORATORY 
Camrriprr, Mam. 

OWQ. NO. 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001529 

SHEET | OF | 



° \ z 

photographk?scale only 


mmww 





























2 





:vsn Mai mg data 


TOTAL NUMBER WINDINGS 6 


WINDING 

NO. 


TURNS 


AWG WIRJL TYPE OF [.'WlMDIfclG 


LEAD S 


SIZE 




START 



FINISH 


2 


WINDING LRESlSTAKlCC LC&iTH I S1Z.E 


RANDOM 


RANDOM 


RANDOM 

COMMON 


RANDOM 

COMMON 


RANDOM 

COMMON 


RANDOM 

COMMON 


T- INSULATE BETWEEN WIMdiMGS Uo. 1 # Mo. 2 WITH A .005 POLYESTER WASHER \ l - 

' PER MIL-I-G31 TYPE G- , 

2- CORES MUST BE A MATCHED QUAD 
AND TWO PARTS 1001529 BE MADE. ' 

3- WIND WINDINGS OVER. EMTIRJE LENGTH OF CORE. |-— — — -- 

4- TURNS OR TURNS RATIO TOLERANCE il%. 1 SCHEMATIC 

5- (B) DEMOTES THE SAME INSTANTANEOUS POLARITY. | ‘ 



see Mote 5 


lloWDG 


3 O ,0 

7^WDG4j8 


s^wDGy 


JORE I 


.CORE 2 


|5WDG 162 36WDG 264 



.480 DIA 
MAX 


re 


POLYESTER. 

WIR.E __ 

CORE 


NOMENCLATURE 
OR DESCRIPTION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M IT 

INSTRUMENTATION LAG 
CONTRACT 


approvco for MSC 


11000285 


APPLICATION 


NONE 



I0067lt-2g 

1010688-1 

PART Of) 
WCNTIFVING NO. 


SEE tlOTE I 
SEE DATA 
see Mote 2 


VtCIFICATION 


LIST OF PARTS AND MATERIALS 

CORE a COIL 
ASSEMBLY 
(REACTOR 1ST STAGE 
MATCHED PAIR) 


CODE IDENT. 


tNSTRUM ENTATtOM 
LABORATORY 
Cammiqm. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001529 
















































































































I WINDING. DATA - 

TOTAL NUMBER WINDINGS 4 


WINDING . 
NO. 

TURNS 

AWG WIRE. 

' SIZE 

TYPE OF 
WINDING 

WINDING 
RESISTANCE. , 

OHM$tZO%6)25C(££f) 

; . LEADS I 

LOJGTH 

SIZE 

IDENTIFICATION I 


START 

FINISH 

1 

150 

r 36 

RANDOM 

3.6 

6* - 

AWG 30 

i 

2 

2 

150 

36 ' 

RANDOM 

3.6 





3 

4 

3 

1900 

£. 4-1 * 

RANDOM 

COMMON 

„ 190 





5 

6 

4 

300 

.... 4-t 

RANDOM 

COMMON 

40 


f : : 

_j 

l _ 

7 

8 


notes: 

I - 

2 - 

3 - 

4 - 


5 - 

6 - 
7- 


8 - 


9- 


INSULATE BETWEEN WINDINGS NO. I a NO. 2 WITH A 005 POLYESTER WASHER PER MIL-1 -631 TYPE G. 

TURNS OR TURNS RATIO TOLERANCE ti% * 

WIND WINDINGS OVER. ENTIRE LENGTH OF CORE 
PREHEAT WINDING AND IMPREGNANT TO 250°F, IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24HRS AT I80°F. - — 

(■) DENOTES THE SAME INSTANTANEOUS POLAR.ITV .. 

WIPE IMPREGNATION DURING CURING CYCLE. 

THE RESISTANCE BErtNcEt/M a/d/NgS S///U-L t/or BE CESS - C 

THAN to MEGOt/MS WUcN MEASURED AT ESOI/OC AETER 
INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A MINIMUM 
OF 5 DAYS PER ND-I002209.C0RE MUST MEET PERFORMANCE I 
REQUIREMENTS OF SCD 1010689 AFTER TEMPERATURE CYCLING. 


SEE NOTE 5 





UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 







DO NOT SCALE THIS DRAWING 


1000285 

MATERIAL: 

NEXT ASSY 

USED ON 

| APPLICATION 


INCHES 
I . I » J . j.... 


0 » - 
PHOTOGRAPHUfStt 


DESCRIPTION 


REVISED PER TORR OST 3*r l/z/Wtfl 


IMPREGNANT 

POLYESTER 

wire: (leads) 

WIRE. 

WIRE __ 

CORE _ 

NOMENCLATURE 
OR DESCRIPTION 


10067 ! 1-13 
1006711-22 
1006711-18 

/O/Ofegg -/ 

PART OR 
IDENTIFYING NO. 


AWG 30 
AWG 41 
AWG 36 


SPECIFICATION 


NOTE 4 46 
SEE NOTE! 
SEE DATA 
SEE DATA 
SEE DATA 


MATERIAL 
OR NOTES 


MIT 

INSTRUMENTATION LAN 

CONTRACT 


j PRAWN |/gtA/ 

IAPPROVE*) FOR MSC 


LIST OF PARTS AND MATERIALS 

CORE a COIL 
ASSEMBLY 
(REACTOR 3RD STAGE) 


COOE I DENT. 


NONE 


INSTRUMENTATION 
LABORATORY 
Camwipm. Maw. 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

1001530 

OF | 


SHEET | 






























WINDING. DATA 


TOTAL NUMBER WINDINGS 4 


WINDING „ 
NO. , 

TURNS 

AWG WIRE. 
SIZE 

TYPE OF 
WINDING 

• 

150 

36 

RANDOM 

2 

150 

~ 36 ’ 

RANDOM 

3 

1500 

- 4-1 

RANDOM 

COMMON 

• 4 , 

300 

4-1 ' 

RANDOM 

COMMON 


WINDING RESISTANCE. LOJQTH SIZE 
RANDOM ~ 6“ :AWG30 


LEADS 

1 IDENTIFICATION 
START I FINISH 


notes: 



I -INSULATE BETWEEN WINDINGS NO. I 8 NO. 2 WITH A 005 POLYESTER WASHER 

2- TURNS OR TURNS RATIO TOLERANCE t\% 

3- WI.N0. WINDINGS OVER. ENTIRE LENGTH OF CORE . 

4 -PREHEAT WINDING AND HYSOL TO 250*F. IMPREGNATE WlNDlNG ' 

WITH HYSOL PULL NO VACUUM. BAKE 24HRS AT I80°F. 

5 -(■) DENOTES THE SAME INSTANTANEOUS POLAR.ITV .... 

6- WIPE IMPREGNATION DURING CURING CYCLE. 

7 - tHe resistance BErrtsEN m/oz/ss s/all /or be less / • . 

ZZZ TNaN ZO MEGO//MS WNeN MEASURED AT SOOtfOC AFTER SAAC/ZS 


.40 O.D. 
.22 I.D 


PER MIL-1-631 TYPE G 


SCHEMATIC 

70WDG4Q8 


SEE NOTE 5 


CORE r 


loWDG162 3 


0 6 


CORE 2 



C. 

MAX 


HYSOL. 
POLYESTER 
WIRE (LEAPS) 

WIRE _ 

WIRE __ 

CORE _ 

NOMENCLATURE 
OR DESCRIPTION 


1006711-13 
1006711 "2a 
1006711" 18 
/0/ot&9 -/ 


I I tOCPfTIFYlfS 1 NO. I SPCC>FICATK)W 

LIST OF PARTS AND MATERIALS 


NOTE4 {6 

see HOTEL! 

SEE DATA 
SEE DATA 
SEE DATA 


MATERIAL 
OR NOTES 


_ 1000285 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M I T 

INSTRUMENTATION LAG 
CONTRACT 


F DRAWN |/glA/ 

APPROVE© rOR MSC 


CORE a COIL 
ASSEMBLY 
(REACTOR 3RD STAGE) 


coot I0ENT. 


KlT/IJ. APPROVAL 

WZKVc 


INSTRUMENTATION 
LABORATORY 
_Ca—ripoc. Mam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001530 

1 OF 





































































4 


3 


2 


1 


» 

| REVISIONS Ol 

TZZ? - 

/ " * ” ■ • .. . i 

ZONE 

SYM 

DESCRIPTION 

OATE 

APPROVAL 


A 

REVISED EE A TDRR 0SW& 

u/u/i 



WINDING DATA 


TOTAL NUMBER WINDINGS 4 


WINDING 

NO. 

TURNS 

AWG WIRE 
SIZE 

TYPE OF 
WINDING 

WINDING 

® » E <® .: 
25°C(REF) 

LEAD S 1 

LENGTH 

SIZE 

IDENTIFICATION 1 

START 

FINISH 

1 

160 

. 4* 

RANDOM 

10 

6" 

AWG 30 

1 

2 

2 

160 

■- 


RANDOM 

10 





3 

4 

3 

1200 



RANDOM 

COMMON 

150 

- 


— 


5 

6 

4 

200 


; . 

RANDOM 

COMMON 

22 


t* - 



7 

8 


notes: 

1 - INSULATE BETWEEN WINDINGS NO. I 8 NO. 2 WITH A .005 POLYESTER WASHER x’.d PER MIL-I-631 TYPE G. 

2 - TURKS OR TURNS RATIO TOLERANCE ti% 

3- W1WD WIMDINQS OVER. EMTI R.EL. LENGTH OF CORE 

4- PREHEAT WINDING AND IMPREGNANT TO 250°F. IMPREGNATE WINDING 

WITH IMPREGNANT. PULL NO VACUUM. BAKE 24HRS AT I80°F. - - - ■ - - - 

5- (»)DENOTES THE: SAME INSTANTANEOUS POLARITY' . ... " 

6 -WIPE IMPREGNATION DURING CURING CYCLE. 

T- Ttfe GEstSTAJ/CE ezntfEEtf rtrt/Dft/Gs st/AL.L//or S£ 

; less rt/Atf to mego//ms *///ea/ measi/^ed at 

.. S501/DC AFTER BA&//G L . r ..,.. " 

. 8 - INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS * . 

PRESCRIBED BY MIL'D' 70327 


9-BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A 
MINIMUM OF 5 DAYS PER ND 1002209. 

CORE MUST MEET PERFORMANCE REQUIREMENTS OF 
SCO 1010688 AFTER TEMPERATURE CYCLING 


SCHEMATIC 

T 0 8 


see Note 5 









A/R 

IMPR.EGNAK1T 

1010687-1 


NOTE 4 (<o 


a/r 

POLYESTER 



see note i 

4- 

A/R 

W1R£. (LEADS) 

1006711“ IS 

AWG 30 

SEE DATA 

3 

A/R 

W1B.E 

I00G7M-22 

AWG 41 

SEE DATA 

2 

2 

CORE 

ioio6©a-i 



i 

QTY. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 








DO HOT SCALE THIS DRAWING 


1000285 

MATERIAL: 

NEXT ASSY 

USED ON 


| APPLICATION 



LIST OF PARTS AND MATERIALS 


M I T 

INSTRUMENTATION LAR 
CONTRACT 



_ 

APPROVCO FOR MSC 

1 4 /QjuLk 

mn/iL appro' 


m 


IIT/JL APPROVAL DATE 


CORE a COIL 
ASSEMBLY 
(REACTOR 2ND STAGE) 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


-RTTT- 

INSTRUMENTATION 

LABORATORY 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001531 


SHEET 


MM 


INCHES 

I . i . I . .i -L 
0 I - 

PHOTOGRAPHKf SCALE ONLY ij 



































WIWDI MG “HAT A 


TOTAL NUMBER WINDINGS 5 



LEADS 


IDENTIFICATION 


TART FINISH 


2 



WINDING tiirn«? AWG WIBX TYPE OF WINDING . . 

NO. TURNS I SIZE - WINDING RESISTANCE | LENGTH | SIZE 


RANDOM 


RANDOM 


RANDOM 

COMMON 


RANDOM 

COMMON 


RANDOM 

COMMON 


notes: 

I - INSULATE BETWEEN WINDINGS NO. I 8 NO. 2 WITH A .005 POLYESTER WASHER gg PER MIL-I-631 TYPE G. 

2- TURNS OR TURNS RATIO TOLERANCE ti% 

3- WIND WINDINGS OVER. ENTIRES LENGTH OF CORE 

4- PREHEAT WINDING AND HYSOL - TO 250°F. IMPREGNATE WINDING 

WITH HYSOL PULL NO VACUUM. BAKE 24HRS AT I80°F. •- - - - - 

5 -(■)DENOTES THE SAME INSTANTANEOUS POLARITY . 

6- WIPE IMPREGNATION DURING CURING CYCLE. 

7- TaJE AES tSTAf/CE BETH/EErf A/h/D/a/GS SS/ALL f/or BE -- * -1 

.I LESS Tt/AA/ AO MEGOHMS A/a/Ea/ AfEASi/^EO AT 1 _ SCHEMATIC i 

500VDC ABEEB BAAE/a/G _ - '.''””11. I I 

I ' 

| 9oWDG5olO 1 


see Note 5 


7^NDG4j8 

5^fOG3j6 


CORE r 


.CORE 2 


loWDG 162 30WDG 264 





» 

I 


i^.4 2 _i 

MAX 


HYSOL _ 

POLYESTER _ 

W1R£. (LEADS) 

W1R.E. _ _ 

COR.E 

NOMENCLATURE 
OR DESCRIPTION 


1010687—I 

IOOG7M-IS 
I00G711-22 
1010686-1 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MOTE 4 4G 
SEC WQTE 1 
SEC DATA 
SEE DATA 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MIT 

tNBTNUMENTATION LAB 

CONTRACT 


( drawn 

APPROVED FOR MSC 


LIST OF PARTS AND MATERIALS 

CORE a COIL 
ASSEMBLY 
(REACTOR 2ND STAGE) 


1000285 


COOC I DENT. 


APPLICATION 


NONE — 


INSTRUM ENTATIOtl 
LABORATORY 
Cammiom. Mm 


MANNEO 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA ORAWING NO. 

1001531 




































































































ZONE SYM 


DESCRIPTION 


I REVISED PER TDRR Of3+4 |/V^3| 


WINDING -DATA 


TOTAL NUMBER WINDINGS 5 


WINDING 


SEC I 
SEC 2 
SEC 3 
SEC 4 


TURNS 


TAP i AWGr W1R£. TYPE OF {WINDING 


SIZE 


WINDING 

RANDOM 

RANDOM 

RANDOM 

RANDOM 

RANDOM 




LE.ADS 

-- | IDENTIFICATION 
START I TAP I FINISH 


|AW<q30l 


notes: ' 

r. (ByDENOTES the same Instantaneous polar ity. 

2. PREHEAT WINDING AND IMPREGNANT TO 250°F IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24HRS AT I80°F. 

; 3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4* WIPE IMPREGNATION DURING CURE CYCLE. 

5* TURNS OR TURNS RATIO TOLERANCE ±1%. 

6 . T//E RESISTANCE BEEh/EEA/ Hf/SD/MSS Sa/alL A/or BE 
LESS TA/AA/ fOAAEGOA/t*S H/a/E*/ MEASt/A?££> Ar 

250 Voc affer baataa/g; " 

?. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

8. BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A 
MINIMUM OF 5 DAYS PER ND-1002209. CORE MUST MEET 

PERFORMANCE REQUIREMENTS OF SCO 1010689 i- 

AFTER TEMPERATURE CYCLING. . , 


SEE MOTE 1 


SCHEMATIC I 

SEC I SEC 2 SEC 3 SEC 4 I 
3 4 5 6 7 8 9 10 II12 13 14 I 


t 

\ 


.50 DIA 
MAX 



~~*J MAX |* | 


A/R IMPREGNANT 
A/R WIRE CLE.ADS) 
A/R WIRE 

a/r wire: 

I CORE 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


1010637-1 

1006711-13" AWG 3(T 
1006711-21 AWG 39 
1006711-22 AWG 4l" 
10106e9-l 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


N0TE244 5 
SEE DATA 4- 
SEE DATA 3 
SEE DATA 


MATERIAL 
OR NOTES 


1000285 



UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


00 NOT SCALE THIS DRAWING 


M I T 

INSTRUMENTATION LAG 
CONTRACT 


I APPROVtO FOR MSC 


LIST OF PARTS AND MATERIALS 

CORE a COIL 
ASSEMBLY 

(TRANSFORMER,POWER} 




CODE IDENT. 


HT/IL approval 


NONE 


INSTRUMENTATION 

LABORATORY 

ammpw. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001532 

























B 


ZONE 


WINDING DATA 


1 V I 1— • * 

WINDING 

TURNS 

TAP 

AWG WIRE 

TYPE OF 

TOTAL WINDING 
RESISTANCE , 

0Hi)5-20% £25 C(EEFj 


in 


LE 

m 

ADS 

IDENTIFICATION 

NO. 

AT 

SIZE. 

WINDING 

Lk.NL) i n 

— 

START 

TAP 

FINISH 

PRI 

600 


4-1 

RANDOM 

39 

6" 

AWG 

30 

i 


2 

SECI 

240 

120 

4! 

RANDOM 

12 





3 

4 

5 

SEC 2 

700 

350 

4-1 

RANDOM 

47 





6 

7 

8 

SEC 3 

240 

120 

4-1 

RANDOM 

12 





9 

10 

II 

SEC 4 

300 

150 

39 

RANDOM 

6.5 


L_ 


L_ 

12 

13 

14 


notes: 

!.(■) DENOTES THE SAME INSTANTANEOUS POLARITY. 

2. PREHEAT WINDING AND IMPREGNANT TO 250°F IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24HRS AT 180 F. 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE ±1%. 

e. Tf/E RESISTANCE BETrfEE// V\//Vp//ZGS Sf/ALL fi/OT BE 
LESS T//AJZ /OM£GO/ZmS lA/f/E/Z A/tEASl/REE> AT 
250 I /DC AFTER BAAT/a/G. 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

8. BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A 

MINIMUM OF 5 DAYS PER ND-1002209. CORE MUST MEET 
PERFORMANCE REQUIREMENTS OF SCD 1010689 ' f~ 

AFTER TEMPERATURE CYCLING. 


SEE. NOTE I 


REVISION S 
DESCRIPTION 


REVISED PER TDRR 0E3M 


B 


REVISED PER TDRR 11653 




DATE 

i/ufc% 


APPROVAL 


~W- 

SieSri 


--1 

SCHEMATIC ' 

SEC I SEC 2 SEC 3 SEC 4 

3 4 5 6 7 8 9 10 II 12 13 14 

- 9 9 9 


njimu 


UduU 



“T 

.50 DIA 
MAX 

__L 


.30 

MAX 


__I 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 







DO NOT SCALE THIS DRAWING 


1000285 

MATERIAL: 

NEXT ASSY 

USED ON 


APPLICATION 


B 


A/R 

IMPREGNANT 

1010657- 1 


NOTE 2< 4 

5 ■ 

A/R 

WIRE (LEADS) 

1006711-13 

AWG 30 

SEE DATA 

4 

A/R 

WIRE 

1006711-21 

AWG 39 

SEE DATA 

3 

A/R 

WIRE 

1006711*22 

AWG 41 

SEE DATA 

a 

1 

CORE 

1010669- 1 



t 

QTY. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 


LIST OF PARTS AND MATERIALS 


M I T 

INSTRUMENTATION LAB 

CONTRACT 


APPROVED. 




m 


PATE 

r/z jl 


Vo-t 6i 


V-Z9 <3 


approved por MSC 
IrtT/IL appro 


m 


fOi 


CORE a COIL 
ASSEMBLY 

(TRANSFORMER, POWER - ) 

UNIT WT. | CODE IDENT. 


SCALE 

NONE 


M i t .— 

INSTRUMENTATION 
LABORATORY 
Camrrioor. Ma—■ 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001532 


SHEET | 


OF | 


1 


1001532 


















REVISIONS 


B 


WINDING DATA 


TOTAL NUMBER WINDINGS 5 


WINDING 

NO. 

TURNS 

TAP 

AT 

AWG W1R.L 

Size 

TYPE OF 
WINDING 

TOTAL WINDING 
RESISTAHCE . 
0^MS-ZC% fiZ5‘C(RL f ) 

.LEADS | 

LENGTH 

SIZE 

IDENTIFICATION I 

START 

TAP 

FINISH 

PRI 

600 


4-1 

RANDOM 

39 

6" 

AWG 30 

i 


2 

SEC 1 

240 

120 

41 

RANDOM 

12 





3 

4 

5 

SEC 2 

700 

350 

4-1 

RANDOM 

47 





6 

7 

8 

SEC 3 

240 

120 

4-1 

RANDOM 

12 





9 

10 

II 

SEC 4 

300 

150 

_i 

39 

RANDOM 

6.5 

_, 

t _ 


t _ 

12 

13 

14 


notes: 

1. v®/ DENOTES THE SAME INSTANTANEOUS POLARITY. 

2. PREHEAT WINDING AND IMPREGNANT TO 250°F IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24HRS AT I80°F. 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE +1%. 

6. 7flE AESiSTAzOcE BEEtt/EEZS tVzz/OZZ/GS Sz/ALL MoT BE 
LESS TZ/AZ/ ZO MEG Oz/MS IAZz/eO MEASi/E ED AT 
250 I /DC AETEH 8AAEZZ/G. 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

8. BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A 
MINIMUM OF 5 DAYS PER ND-1002209. CORE MUST MEET 
PERFORMANCE REQUIREMENTS OF SCD 1010689 
AFTER TEMPERATURE CYCLING. 

9. INDIVIDUALLY INSULATE PRI WINDING LEAD-OUTS FROM 
OTHER WINDINGS AND INSULATE ALL LEAD SET POINTS WITH 
MYLAR TAPE PER MIL-1-15126. 


SEE NOTE 1 


A 

3 


DESCRIPTION 


REVISED PER TDRR 
REVISED PER TD RR 11653 


REVISED PER TDRR 20287 


3M 


25 JUKI 


APPROVAL 



r 



SCHEMATIC 


SEC I SEC 2 SEC 3 SEC 4 
4 5 6 7 8 9 10 I M2 13 14 

ILJUJULRU 


n 


PRI 





UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 








DO NOT SCALE THIS DRAWING 


1000205 

MATERIAL: 

NEXT ASSY 

USED ON 


| APPLICATION 



A/R 


A/R 


A/R 


A/R. 


A/R 


QTY. 

REQD. 


TAPE 


IMPREGNANT 


WIRE (LEADS) 


WIRE 


WIRE 


CORE 


NOMENCLATURE 
OR DESCRIPTION 


1010657-1 


1006 7U -13 


1006711-21 


1002711-22 


1010669- I 


PART OR 
IDENTIFYING NO. 




AWG 30 


AWG 39 


AWG 41 


SPECIFICATION 


NOTE 9 
NOTE 2^4 


SEE DATA 


SEE DATA 


SEE DATA 


MATERIAL 
OR NOTES 


FIND 

NO. 


LIST OF PARTS AND MATERIALS 


M 1 T 

INSTRUMENTATION 

CONTRACT 

r^AS <*453 I 

LAB 

DATE 

APPROVED^ ] 


CHECKED 

p 

fo-i 61 

DRAWN 

ItZ1 


ARRROVEO FOR MSC 

'UJ 3 A < 

BriT/JL APPROVAL 

DATE 

[0 fop , it. 

IP 


CORE a COIL 
ASSEMBLY 

(TRANSFORMER, POWER') 


SCALE 

NONE 


UNIT WT, 


CODE IDENT. 

80230 


MIT 

INSTRUM ENTATION 
LABORATORY 

_CAMimoot, Mass. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001532 


SHEET | 


OF | 


O 


B 


1 


1001532 

















V; 

-''.V 


u 


c 







; ; 1 

TOTAL NUMBER WINDINGS 5 


WINDING -DATA 


WINDING TAP AWG W1R£. TYPE OF WINDING-,-^ 

NO. TURNS AT I . SIZE - WINDING RESISTANCE 1LMGTH SIZE 


LEADS __ 

I IDENTIFICATION 
START I TAP I FINISH 


PRI 

600 


4-1 

RANDOM 

SECI 

240 

120 

4-1 

RANDOM 

SEC 2 

700 

350 

4-1 

RANDOM 

SEC 3 

240 

120 

4-1 

: RANDOM 

SEC 4 

300 

150 

' 39 

RANDOM 


AWG, 30 


notes: 

: f. (•^DENOTES THE SAf^TE lNSTANTANEOUS POLARITY _ I: 

2. PREHEAT WINDING AND HYSOL TO 250°F .IMPREGNATE’ WINDING 
WITH HYSOL ' PULL NO VACUUM. BAKE 24HRS AT I80°F. 

3c WIND WINDINGS OVER ENTIRE LENGTH OF CORE 
4* WIPE IMPREGNATION DURING CURE CYCLE. 

5* TURNS OR TURNS RATIO TOLERANCE+1%. 

6. TtiE RESISTANCE 8£rhfC£// H/ftfD/tfSS Stfai-L Wor BE 
LESS TtfAAf fO MEGOHMS W//£ A/ Af£ASt//?£& AT 
SOOl/OC AFr£X 3A*r/t/G ~~~ 


SEE MOTE I 


SCHEMATIC 

SEC I SEC 2 SEC 3 SEC 4 
4 5 6 7 8 9 10 II 12 13 14 


I 2 
PRI 


.50 DIA 
MAX 




A/R HYSOL _ 

A/R, WIRE CLE.ADS) 
A/R. WIRE 
A/R WIRE 
I CORE _ 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


1010637-1 
100g7ll-t3T 
I00G7U-2I 
1000711-22" 
1010659-1 


I | tOCNTIFriN? NO. | #PeC * FICAT,0H 

LIST OF PARTS AND MATERIALS 


NOTE 24 4 
SEE DATA 
SEE DATA 
SEE DATA 


MATERIAL 
OR NOTES 


I 

I 


5 

5 


__ 1000285 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANQLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M IT 

INSTRUMENTATION LAS 
CONTRACT 

_ ySJjjj 3 | bATE 

APPROVIO 

CHCCKCO Mgj, Vo'*6l 

prawn x.JU b-ey-^3 

APPROVED FOR MSC 

mT/VL APPROVAL DATE 


CORE a COIL 
ASSEMBLY 

(TRANSFORMER,POWER} 


SCALE 

NONE 


COOE I0ENT. 


INSTRUMENTATION 

LABORATORY 

Campriopb. Mam. 

dwq. no. 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001532 

SHEET Of 










































































































































RG AND R7 70 BE SC.LE.CTED AT TEST 
RANGE OF VALUES FROM /§ H THRU E4.9K ON MS 

RIO TO BE SELECTED AT TEST 

RANGE OF VALUES FROM /OK THRU 24. 9K OHMS 
Rt3 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM SK THRU 6 K OHMS 
R/4 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM /OHM THRU tO OHMS 

N/NDING RES/STANCE FOR ACCEPTANCE TEST/NG J 
CONTROL IN/NDING /95 tESOHMS 
TERMINALS 3 AND 4 

R3 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 300H THRU /MEG OHMS 

Ct TO BE SELECTED AT TEST 

RANGE OF VALUES FROM JO THRU t<40 UFO 


I a L2 1001528 REACTOR ASS T 

L3 100 15 31 REACTOR 

L4_ 1001530_REACTOR _ 






























































8 


6 


5 



SQUARE WAVE 


notes: 

1. INTERPRET CRAW/MG IN ACCORDANCE WITH STANDARDS PRESCRIBED SY 
MIC - O - 7032 7 

2. UNLESS OTHERWISE INDICATED 

ALL RESISTOR VALUES ARE /N OH‘ *5 
ALL CAPACITOR VALUES ARE /N OP’D 

3. R2 TO BE SELECTED AT TEST 

RANGE OF VALUES FRONT 40.2K THRU I2/K OHMS 

4 RG AND R7 TO BE SELECTED AT TEST 

range of values front is k thru 24. 9kohms 

5. RIO TO BE SELECTED AT TEST 

RANGE OF VALUES FROM /OK TNRU 24 .9 K OHMS 

6. R!3 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 2K TNRU QKOHMS 

7. R14 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM / OHM THRU fO OHMS 

Q. W/ND/NG RESISTANCE FOR ACCEPTANCE TESTING .* 

CONTROL W/ND/NG 195 t£5 OHMS 
TERMINALS 3 AND 4 

9. R3 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 300K THRU I MEG OHMS 

to. Cf TO BE SELECTED AT TEST 

RANGE OF VALUES FROM JO THRU 140 UED 


8 


6 


5 


i 


OVDC 



Rl 

60.1K. 

WV— 


S RI2 
>I5K 


HZ 113 K 
UUULXJUUJ 


PI6 1 


"i TCRI2 1 

FCRI3 

432 

LC2 

'1.0 

CRI4(] 

d 

6 7 

uuulTjuuu 

8 




<D 


OUTPUT 
> TO 
2NI724 


| REVISIONS O 3 ft* I I 

ZONE 

SYM 

DESCRIPTION 

r DATE 

WS32M\ 


A 

R£l-VS£D PE* TCP* 

nfit/ki 

jJL- J 


3 

REVISED PER TDRR 11654 

5 


C 

PEV/SED P£/P W £073Z 

•4 Juc 

65 





1 

1 


C 


<D 


/ 


REF 

DES 

PART NO. 

DESCRIPTION 

VALUE 

T0L 

RATING 

Rl 

1010694 

-302| 

RESISTOR 

68. IK 

t 1% 

I/I0W 

P2 

1010694 

RESISTOR NOTE 3 

SA 

• T 



I/IOW 

R3 . 

ICM0693 

RESISTOR a tore 9 

S.A 

.T 



»/4-W 

R4 

1010694-126 

RESISTOR 

IK 



■Smi 

R5 

1010694-96 

RESISTOR 

487 



B 


R6 

1010694 

RESISTOR NOTE 4 

S A.T 



B 


R7 

1010694 

RESISTOR Note 4 

S-A.T 



B 


R8 

:3!0£?4-?6 

RESISTOR 

487 



Bi 


RE 

1010^94-126 

RESISTOR 

IK 



_ 


RIO 

1010694 

RESISTOR Note 5 

S.> 

A.T. 



HbI 


Rl 1 

1010694-67 

RESISTOR 

243 



B 


RI2 

1010694-143 

RESISTOR 

I.5K 



B 

hi 

RI3 

1010694 

RESISTOR NOTES 

S.A.T. 



BHaoB 

RI4 

1010604 

RESISTOR NOTE 7 

S. A.T 



BBWI 

RI5 

1010695- 56 

RESISTOR 

196 



■2SBI 

RI6 

1010695-91 

RESISTOR 

432 


f 

mem 

Cl 

1006789 

CAPACITOR mote 10 

5 A T 

to v. 

WKSMM 

C2 

1006755-^9 

CAPACITOR 

1.0 

10% 


C3 

1006755-19 

CAPACITOR 

3.3 

10% 

mmm i 

_C4_ 

1006755*19 

CAPACITOR 


mssEM 

15V 

CRI 

1010497 

DIODE 

iS 


3.4 W 

CR2_ 



DIODE 



mam 

Hb 

■hi 

CR3 



DIODE 






CR4 



DIODE 






CR5 



DIODE 






CR6 



DIODE 






CR7 



DIODE 






CR8 



DIODE 






CR9 



DIODE 






CRIO 



DIODE 






CRI 1 



DIODE 






CRI2 



DIODE 

IHH 

IHHI 

IHi 

IHH 


CRI3 


t 

DIODE 

IflK 

'SHI 

mm 

in 


CR.4 

1010236-2 

DIODE 

IN 9 53 3 

mm 








LI 9 L2 

1001528 

REACTOR ASS'Y 




L3 

10015 3 

REACTOR 




L4 

1001530 

REACTOR 










Tl 

1001532 

TRANSFORMER 







1000285 


UNLESS OTHERWISE SPECIFIED 


OtMlNSlONS ARE 
TOLERANCES ON 
FRACTIONS 


00 NOT SCALE THIS DRAWING 


LIST OF PARTS AND MATERIALS 






Ka l/w 5 


..miovco ro« MSC 

iq-^-un 




1M L 


SCHEMATIC 

H temperature control 

AMPLIFIER 


SPACECRAFT CENTER 
HOUSTON Tt>AS 


NASA DRAWING NO 

1001533 


i« 



3 


1001533 







































SQUARE WAVE 


NOTES: 
I. 


INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY 
MID-D - 70327 

2. UNLESS OTHERWISE INDICATED: 

ALL RESISTOR VALUES ARE iN OHMS 
ALL CAPACITOR tVALUES ARE /N UFD 

3. RE TO BE SELECTED AT TEST 

RANGE OP VALUES PROM 40.2 K THRU 12IP OHMS 

4 RG ANO R7 TO DESELECTED AT TEST 

RANGE OP VALUES PROM 15 TC thru 24.9NORMS 

5. RiO TO BE SELECTED AT TEST 

RANGE OF VALUES PROM /OIK THRU 24. 9IK OHMS 

6. R!3 TO BE SELECTED AT TEST 

RANGE OP VALUES FROM 2 IK THRU 3 IK OHMS 

7. R14 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM /OHM THRU tO OHMS 

0. WINDING RESISTANCE FOR ACCEPTANCE TESTING .* 

CONTROL WINDING 195 125 OHMS 
TERMINALS 3 AND 4 

9. R3 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 300IK THRU /MEG OHMS 

10. Ct TO BE SELECTED AT TEST 

RANGE OF VALUES FROM JO THRU 140 UFO 






X 


1001533 







































notes: 

I. INTERPRET CRAW/N 6 IN ACCORDANCE /V/TH STANDARDS RRESCR/&ED BY 
M/L.-0- 70327 

£. UNLESS OTHERP//SE /ND/CATEDt 

ALL RES/S TOR VALUES ARE IN OH,MS 
ALL CAP AC,TOR. VALUES ARE /N UFD 

3. R2 TO HE SELECTED AT TEST 

RANGE OF VALUES FROM 40.2K THRU ,'2/K OHMS 

4 RG AND R7 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM f5 H THRU 24.9KOHMS 

5. R/C TO BE SELECTED AT TEST 

RANGE OF VALUES FROM /OK THRU 24.9K OHMS 

6 . R!3 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 2K THRU QKOHMS 

7. R!4 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM /OHM THRU tO OHMS 

6 . W/NDING RES/STANCE FOR ACCEPTANCE TEST/NG .* 

CONTROL IT/.’ND/NG 195 125 CHMS 
TERMINALS 3 AND 4 

9. R3 TO 8 E SELECTED AT TEST 

RANGE OF VALUES FROM 300* THRU /MEG OHMS 


10. Cl TO SC SELECTED AT TEST 

RANGE OF VALUES FROM JO THRU 140 UFD 


3 


2 


1 


L 



T 


1 


1 


OVDC. 


\ 



CRIO 


OUTPUT 


RI4 

NOTE 7 


<2) 


> TO 
2N/724 


<*>J 


1 


| REVISIONS O *5 EG f | 

ZONE 

SVM 

DESCRIPTION 

DATE 

APPROVAL 

t 

A 

REV'S£D PER TERR 05**1 

ll/ft/iS 

llK 


3 

REVISED PER TDRR //6S4 



±J 

PEV/SED P£A> TM># £073Z 

14 Jul 


0 | EE//SE/> PEP TOPE EIE74 

30 Ju 


£ 

&//SE2? 7D22 2/5/J/ 







CRII 


REF 

DES 

PART NO. 

DESCRIPTION 

VALUE 

T0L 

RATING 

Rl 

I0IO69A-3C2 

RESISTOR 

68. IK 

t 1% 

I/I0W 

R2 

10(0694 

RESISTOR NOTE 3 

SAT 



:/;ow 

R3 

1010695 

RESISTOR More 9 

S.A.T 



*/4- W 

R4 

ICI0694-I26 

RESISTOR 

IK 



1/IO Vi 

R5 

1010694-96 

RESISTOR 

487 





R6 

1010694 

RESISTOR NOTE 4- 

SA.T 





R7 

10106 94- 

"resistor Note 4- 

S- 

A.T 





R8 

7df0694-?4 

RESISTOR 

487 





R9 

(010694-126 

RESISTOR 

IK 





RIO 

1010694- 

RESISTOR Note 5 

S.A.T. 





Rl 1 

1010694-67 

RESISTOR 

24-3 





RI2 

1010694-143 

RESISTOR 

I.5K 





RI3 

1010694 

RESISTOR NOTE 6 

S.A.T. 



I/I0W 

RI4 

I0I0C04 

RESISTOR NOTE 1 

5., 

A.T 



IW 

RI5 

10(0695 -58 

RESISTOR 

196 



I/6W 

RI6 

1010695-91 

RESISTOR 

432 


r 

I/8W 

Cl 

1006 73 9 

CAPACITOR H0TE 10 

5 A T 

10 v. 

6 V 

C2 

I0067f5 -69 

CAPACITOR 

1.0 

10 % 

35 V 

C3 

(006755-19 

CAPACITOR 

3.3 

10 % 

15V 

_C4 

IOC6755-19 

CAPACITOR 

3 3 

10 V. 

15V 

CRI 

1010497 

DIODE 

5CO PI V 


3.4. W 

CR2 



DIODE 






CR3 



DIODE 


_ 




CR4 



DIODE 






CR5 



DIODE 






CR6 



DIODE 






CR7 



DIODE 






CR8 



DIODE 






CR9 



DIODE 






CRIO 



DIODE 






CRI 1 



DIODE 






CRI2 



DIODE 






CRI3 



DIODE 





, 

CRI4 

1010830-2 

DIODE 

IN958 E 

57. 

4-00 

VfLV 







LISL2 

1001528 

REACTOR ASS’Y 




L3 

10015 31 

REACTOR 




L4 

1001530 

REACTOR 










Tl 

1001532 

TRANSFORMER 






UNIFSS OTHFPWWf SPECIFIED 


DIMENSIONS ARC IN INCHES 
TOLERANCES ON 

FRACTIONS OCCIMALS ANGIES 


DO NOT SCALE THIS DRAWING 


SPECIFICATION 


LIST OF PARTS AND MATERIALS 


INGTNUMLNTATION LAN 

NAS.9J 


i^s2 


$ys? : nm 


I /-•' # 




AWROVtO TOR MSC 
MlT/IL APPROVAL 


l3 








SCHEMATIC 
TEMPERATURE control 
AMPLIFIER 


SCALE 


NASA DRAWING NO 

1001533 


i 


C 


B 


A 


1 

I 


II 

|1 


3 


2 


1 


1001533 E 































MLEWSiaS&i} i.J l *J l, « 1 i'L 'Sim 





































































































































ZONE SYM 



A I/t ’ZJ//SC.D FEJ* rDRFt OS 3H3 I It/**/* 


2T3) 7 PLACES 


I 2 3 4 5 6 7 

© @ © © © © © 



.040 MAX 



E 

II 


E 


notes: 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL'D* 70327 

2. SOLDERING PER MIL*S"6872A WITH SN50WARP2 
1 SOLDER PER QQ-S‘571 


A/R SOLDER _ 

7 TERMINAL 
I COVER MACHINED 


NOMENCLATURE 
OR DESCRIPTION 


1010690" 1 
1001539 1 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


I SEE note; 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M I T 

INSTRUMENTATION LAS 
CONTRACT 


PRAWN 1 
APPROVED FOR MSC 


1000285 


LIST OF PARTS AND MATERIALS 

COVER 

ASSEMBLY 

ALE I UNIT WT. I CODE IDENT. 


WT/IL APPROVAL 


INSTRUMENTATION 
LABORATORY 
Camriow, Maw. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001534 


APPLICATION 




PH0T0GRAP«<f SCALE ONLY 























2 

















































m 


LI REF 


ce / kr/’fl i« , 9l 


RED-4 


RED-2 


R3 

SEE 

NOTE 4 TI-4 


RI4 r- 

SEE 

NOTE 4 TERM-5 L4-6 


-TERM 6 


€*r\ \cea\ 


L3-6- 

Cl(-) -<- 

SEE NOTE 4 


GRN-2- 




6RN-4 



-TI-I3 
-—►T I—10 


-6RN-T 


iGLl I 


•Cl(+) 


,▼ t \ \ TI-7 L3-7 
L3-4 L4-|3 l4 T . 3 

T Tl — 14 L4 a * L4 

L3-2 TH2 „ 


RED-9 


~ r \ ee ]Tl-8 I 

■= t SEE. NOTE 1 T 

L4-8 4 „ t R2 

; TI-6 SEE NOTE 

I T 4 

-►R7 L4-5 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

2. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE 
WITH MIL- STD-440, WITH SN60 WARP2 SOLDER PER QQj-S-571.. 

3.1/5E A7FACAfcD LEADS. - : 

4. FOE If/FOEMAT/O// EE&AED/a/G R£> E<o t E 7, E/0 > Et3, R!4, E3 4 C/ 
SEE A/OFES QfJ DRAW/A/6 1000£85. —— - -- - 


REVISIONS QZSfrl 


ZONE I STM 


DATE I APPROVAL 


A I REVISED PER TDRR 053*1 


L4 REF 


L4-4 


1OL . G 


ADDITIONAL 
CONNECTIONS 
RED-5 (Ll-5)|TERMINAL 3 

RED-10 (LI-10) R6 __ 

RE0-I2 (LI-12) R2 
GRN-5 (L2-5) TERMINAL 4 
GRN-IO (L2-I0) R7 

L3-7 _RIO__ 

L4-7 _ m3_ 

Tl-I TERMINAL I 

TI-2 _ TERMINAL 2 

TERMINAL 7 RI4 _ 

RED-1 (Ll-I) TI-5 

RED-3 (LI-3) TI-3 _ 

TI — II _ L3-I _ 

Tl— 9 _ L3—3 _ 

RED7 (LI-7) R3_ 


SEE NOTE 3 


SEE NOTE 3 


\a/e\ ns/xc 


lO067//-/3\ AWG 30 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


LIST Of PARTS AND MATERIALS 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS OECIMALS ANGLES 


M I T 

INSTRUMEi 'TATION LAS 
CONTRACT 


INSTRUM ENTATION 
LABORATORY 

CaMDWIPNC. Maw. 


WIRING ASSEMBLY 


DO NOT SCALE THIS DRAWING 


[ DRAWN | 

APPROVED JO* MSC 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


1000285 


NASA DRAWING NO. 


CODE IOENT. 


'MIT/IL approval 


1001535 


APPLICATION 




INCHES 


0 » z r; 

photographkTscale only ^ 





























notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

2. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE 
WITH MIL-S-6872 WITH SN60 WRAP2 SOLDER PER QQ-S-571. 

3. Use attached leads. 

4-. FOR If/FORMAT/O/Z R£GARD/a/G RE, RG, R7, R/O, R/3, F/4, £3 d C/ 
SEE AZOTES OfZ DRAW//ZG /OOOE85- 


SEE NOTE 3 


B 



ifll SgSIOOl 


















ZONE I SYM 


REVISIONS 


DESCRIPTION 


DATE I APPROVAL 


LI REF 


cei WA ce 9 


RED-4 


RED-2 



RED-7 TI-4 L3-5 


TERM-7 TERM-5 L4-6 


L4 REF 


► TERM G 

-TI-I3 

N-TI-IO 

—*-GRN-7 


+ 1 

Icvrrl lew I 
1 L4-4 


GRN-2- 
GRN-4« 


V $RJCL 


. ’ t \ ♦ TI-7 L3-8 
L3-4 L4-IJB L4 l 3 J 

. yTI-14 a’ L 4 

L3-2 TI-12 ,, 

RED-9 


,RI4 1 j RI2; 


ADDITIONAL 

CONNECTIONS 


ee | TI-8 i 

t SEE NOTE I T 

L4-6 ® t R2 

TI-6 SEE NOTE 3 


notes: 

I- INTERPRET DRAWING IN ACCORDANCE WITH MIL - 0*70327 
2. USE SOLDER SN60 PER QQ-S-571. 

.3.//SE ATTACHED LEADS i::, Z _ I ” ^ — 

4. FOR Ia/EORMAT/O// A£&AftD///G /?<?> /?6, E7, H/0 > fit5 4 Ht+ 
SEE MOTES Ot/ DEAW/A/& IOOOE3S -- 


RED-5 

RED-10 

RED-12 

GRN-5 

GRN-IO 

L3-7 _ 

L4-7 _ 

Tl-I 

TI-2 _ 

TERMINAL 4 
RED-1 

RED-3 _ 

Tl-ll _ 

TI-9 


TERMINAL 3 

R6 

R2 

Rl _ 

R7 

RIO _ 

RI3 _ 

TERMINAL I 
TERMINAL 2 

m_ 

TI-5 _ 

TI-3 _ 

L3-I _ 

L3-3 


SEE NOTE 3 



SEE NOTE 3 


\A/E\ tV/£C 


NOMENCLATURE 
OR DESCRIPTION 


_ /0/O67//-/3 _ 

I IDENTIFYING* NO. SPECIFICATION 

LIS T OF PARTS AND MATERIALS 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 


M I T 

INSTRUMENTATION LAS 


_ 1000285 

NEXT ASSY USED ON 

APPLICATION 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

APPROVED 

CONTRACT 

T5XTT 


CHECKED 


JJZTs 


— DRAWN 

I *U‘J 

7-/7-U 

DO NOT SCALE THIS DRAWING 

APPROVEO 

Sf* MSC 


MATERIAL 

"6)96 

Ifa/b-. 

2 -(.y 


WIRING ASSEMBLY 


CODE IDENT. 


'mit^il approval 

'LL 


INSTRUMENTATION 
LABORATORY 
Camwiow Ma—. 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

1001535 

SHEET OF 





























































.82 

.78 


I 

I 


il 



NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 

2. BREAK ALL SHARP EDGES .010 MAX. 























































3 


. _ REVISIONS __ 

& Z0NE SYM _ DESCRIPTION DATE | APPROVAL" 

A REVISED PER TDRR 053** nyit/a] UJIr^ 



2 PLACES 


1 SEE KlOTE Z, 

2 PLACES . 



,25 ±.03 


SEE NOTE 3 


NOTES. 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. BRAZE PER MIL-B-7883 WITH CLASS4 SILVER SOLDER PER QQ-S-561. 

3.SURFACE TO BE FLAT WITHIN .015 T.I.R.. 

4. FINISH - TIN PLATE PER MIL-T-10727 TYPE IT (HOT DIP). 

5. PAN HEAD SCREW, CRES,#4-40 NC-2A X 5/16 LG PER MS 35233-14. 


CASE ~ MACHINED 
SCREW_ 


NOMENCLATURE 
OR DESCRIPTION 


1001536 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


SEE NOTE! 

MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS OECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M I T 

INSTftUMKNTATION LAB 
CONTRACT 

NAS *1*3, I-BaTT 


I drawn I gJJ 

APPROVED FOR MSC 


1000285 


LIST OF PARTS AND MATERIALS 


CASE ASSEMBLY 


CODE IDENT. 


RIT/U. APPROVAL 


INSTRUMENTATION 
LABORATORY 
Camrrio—. mars. 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

1001537 


APPLICATION 


1 
























ZONE SYM 


REVISIONS 

DESCRIPTION 


/ O S 61 _ 

I DATE | APPROVAL 


2 PLACES 


::5ee xJote a 

2 PLACES 



.25 4.03 


SEE NOTE 3 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. BRA2E PER MIL-B-7883. 

3.SURFACE TO BE FLAT WITHIN .015 T.I.R.. 

4. FINISH - TIN PLATE PER MIL-T-10727 TYPE IE (HOT DIP). 

5. PAN HEAD SCREW, CRES,#4-40 NC-2A X 5/16 LG PER MS 35233-14. 


CASE - MACHINED 
SCREW _ 

NOMENCLATURE 
OR DESCRIPTION 


1001536 


SEE NOTE 5 I 


I I | SPECIFICATION 

LIST OF PARTS AND MATERIALS 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 


M I T 

INSTRUMENTATION LAS 


_ 1000285 

NEXT ASSY USED ON 

APPLICATION 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

CONTRACT 

NAS 

APPROVED 

DATE 



CHECKED /!. 


DO NOT SCALE THIS 

DRAWING 

— DRAWN €jj 

__ approved tor M3C 

7-/S-63 

MATERIAL 



7-67 



iKit/il approval 

f DATE 


CASE ASSEMBLY 


CODE tOENT. 


INSTRUMENTATION 

LABORATORY 

Cawdripdk. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001537 

SHEET OF 






















































4.00 

PHOTO REF 




APPLICATION 


2 



















































































REVISIONS 


M ZONE SYM 


DATE I APPROVAL 


A \REi\//S£.D PEA rDX* 04532* 


;|| 4 PLACES 



SEE NOTES 3 84 


.560 BSC 


.150 BE>C- 


. I_2 _ 3_4 5 6—7__i 


133 tool DIA THRU 7M0LES 

I&J0I5 Dl/T) 


-.23 R 4 PLACES 


.203 BSC 6 PLACES 


4 PLACES 


I I I I I I 


r ■ 



NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. FINISH-TIN PLATE PER MIL-T-10727. TYPEH (HOT DIP). 

3. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

4. ENGRAVE OR STEEL STAMP PER ND1002019 (.09 HIGH CHARACTERS.) 

5. BREAK ALL SHARP EDGES .010 MAX. 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


1000285 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 

MATERIAL: .020 CRES. 
=jrHARD PERQQ-S-636 
COND. 2 


M I T 

INSTRUMENTATION LAB 
CONTRACT 


LIST OF PARTS AND MATERIALS 


COVER-MACHINED 


CODE I DENT. 


INSTRUMENTATION 

LABORATORY 
Cawhipa*. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001539 




■WJL-El. in 




























































3 


2 


oMki 


ZONE SYM 


DESCRIPTION 


DATE | APPROVAL 


_A _ REVtSCD P£B rOKH 04-532. /A4-*3 yj | 

B ppy/seo />&t row oSzS'O _ iifu/it 


4 PLACES 


4 PLACES 



-BEND RELIEF AS REQUIRED 
8 PLACES 


SEE NOTES 384 


' .560 BSC 


.1_2 _3_4_5_6_ '( 


.150 BSC 


/.■ 


• l33 -002 D,A THRU 7H0les 


-.23R 4 PLACES 


.203 BSC 6 PLACES 


4 PLACES 


I I I • I I 


—U I 4_|——I—h 
| • * * ; « * 


notes: 

I. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL~D-70327 
• 2.FINISH-TIN PLATE PER MIL-T-10727. TYPEH (HOT DIP). 

5.CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. , 

4. ENGRAVE OR STEEL STAMP PER ND1002019 AND 
ND 1002122, TYPE H, CLASS I, .09 CHARACTERS 

5. BREAK ALL SHARP EDGES *010 MAX 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


10015 34 1000285 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGUS 


DO NOT SCALE THIS DRAWING 

MATERIAL: .020 CRES. 

^ HARD PERQQ-S-636 
C0ND.2 


M I T 

INSTRUMENTATION LAB 
CONTRACT 


LIST OF PARTS AND MATERIALS 


COVER, MACHINED 


CODE IOENT. 


RT/IL APPROVAL 


INSTRUMENTATION 

LABORATORY 

Cammiom. Mam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001539 

!T I or | 




























i 


B 


§5 4 PLACES 


MUC.D -1 

14 I 

in—I i — 


“i 


1.125 
1.115 JT 


.560 BSC 


1.53 


1.52 


.27 

'.23 


4 PLACES 




. I_2 __ 3_4_5_6—7_ 



i_ kL 


.150 BSC 




■BEND RELIEF AS REQUIRED 
8 PLACES 


SEE NOTES 3 84 



133 -002 DIA THRU 7 H0LES 


#>.030 DIA 


.25 R 

.23R 4 PLACES 


.203 BSC 6 PLACES 


SYM 


POISED PEP PDPp 04-532. 


6 


DIM 


DESCRIPTION 


PP//3£0 £>£* rPPR OS150 


IL6-&3 

n/u/cs 


REV/5E0 PER TDRR //6SQ 






APPROVAL 


wi l_ 


.08 

.04 


4 PLACES 


+ rrJ 

i i ~ 

_ 1 _ ^ 

■ i_ i_ 






— 


— 

n 

J 1 11 

1 


notes: . 

1. INTERPRET DRAWING IN'ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL'D’70327 

2. FINISH - TIN PLATE PER MIL-T-10727. TYPE H (HOT DIP). 

3. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

4. ENGRAVE OR STEEL STAMP PER NDI0020I9 AND 
ND 100212 2, TYPE H, CLASS I, .09 CHARACTERS 

5. BREAK ALL SHARP EDGES .010 MAX 


1001534 


1000285 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MATERIAL: jJ^O CRS. 

p HAND PERQQ : S'636 
C ON'D.2 


QTY. 

REQD. 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


FIND 

NO. 


LIST OF PARTS AND MATERIALS 


M 1 T 

INSTRUMENTATION 

CONTRACT 

LAG 

DATE 

APPROVED P 

A*'? C: 

CHECKED 



DRAWN 

PJJ 


APPROV CO FOR MSC 

6(y\L APPROVAL 

DATE 

W/Ca/j^v %&. 



COVER, MACHINED 


SCALE 

2/1 


UNIT WT. 


CODE IDENT. 


-HTT- 

INSTRUM ENT ATION 
LABORATORY 
Cammipoi, Mam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001539 


SHEET 


I OF | 


B 


1001539 C 



































' ' ; 4 ’' 


• *■ 

I*: 

fe,": 


'Its-:'' . 





4 PLACES 



.560 BSC 


.150 BSC- 


. I_ 2 _ 3_4_5_6_7_! 


.203 BSC 6 PLACES 


4 PLACES 


• • i > i i 


r 



. i • • 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. FINISH-TIN PLATE PER MIL-T-10727. TYPEH (HOT DIP). 

3. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

4. ENGRAVE OR STEEL STAMP PER NDI0020I9 (.09 HIGH CHARACTERS.) 

5. BREAK ALL SHARP EDGES .010 MAX. 


APPLICATION 


SEE NOTES 3 84 


.120 +'qq2 DIA THRU 7 HOLES 

K&J0I5DIA1 


-.23R 4 PLACES 




NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


1000285 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGUS 


DO NOT SC AU THIS DRAWING 

MATERIAL: .020 CRES. 
^HARD PER QQ-S-636 
C0ND.2 


M I T 

mmtUMCNTATION LAG 
CONTRACT 


LIST OF PARTS AND MATERIALS 


COVER-MACHINED 


CODE IDENT. 


INSTRUMENTATION 

LABORATORY 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001539 

























































WINDING DATA 


TOTAL NUMBER WINDINGS 7 


WINDING 

NO* 

TURNS 

AWG WIRE 
SIZE 

TYPE OF 
WINDli,^ 

WINDING 
RESISTANCE 
0HMST20% AT 
25°C (REF) 

LEADS 1 

LENGTH 

SIZE 

IDENTIFICATION | 

START 

FINISH 

1 

400 

41 

RANDOM 

25 

6 IN 

AWG 30 

1 

2 

2 

400 



RANDOM 

25 





3 

4 

3 

400 



RANDOM 

25 





5 

6 

4 

400 



RANDOM 

25 





7 

8 

5 

200 



RANDOM 
COMMON 
TO CORES 

1 82 

25 





9 

10 

6 

200 



RANDOM 
COMMON 
TO CORES 
384 

25 





II 

12 

7 

1200 


i _ 

RANDOM 
COMMON 
TO CORES 
1,2,384 

235 





13 

14 


i 


I. INSULATE BETWEEN WINDINGS NO. 1,2,3 8 4 WITH A .005 POLYESTER 
, WASHER .40 0D/.22 ID PER MIL-I-631 TYPE G 

fc. WIND WINDINGS OVER ENTIRE LENGTH OF CORE « 

3. TURNS OR TURNS RATIO TOLERANCE il% • 

4. CORES MUST BE A MATCHED QUAO- 

5. (■) DENOTES THE SAME INSTANTANEOUS POLARITY 

6. DIRECTION OF WINDING STARTS INSIOE ALL FOUR CORES 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D'70327 

8. SET LEADS EQUALLY SPACED AROUNO PERIPHERTY 
OF WINDING, ORDER OPTIONAL 

9. WIPE IMPREGNATION DURING CURE CYCLE 

10. PREHEAT WINDING AND IMPREGNANT TO 250°F 
IMPREGNATE WINDING WITH IMPREGNANT 
PULL NO VACUUM 

BAKE 24 HRS AT 180*^- 

II. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE 

LESS THAN 10 MEGOHMS WHEN MEASURED AT 250VDC AFTER BAKING 

12. BEFORE WINDING, 

TEMPERATURE CYCLE CORES FOR A MINIMUM OF 5 DAYS PER ND'1002209 
! !■ CORES MUST MEET PERFORMANCE REQUIREMENTS OF SCO 1010688 AFTER 

TEMPERATURE CYCLING 


i r 



f. 























































TOTAL NUMBER WINDINGS 


WINDING DATA 
7 


NOTES 

I* 


B 


INSULATE BETWEEN WINDINGS NO. 1,2,3 a 4 WITH A .005 POLYESTER 
WASHER .40 0D/.22ID PER MIL-I*63I TYPE G 

WIND WINDINGS OVER ENTIRE LENGTH OF CORE SEE NOTE 5 

TURNS OR TURNS RATIO TOLERANCE 1 1% • 

CORES MUST BE A MATCHED QUAD- 
(■)DENOTES THE SAME INSTANTANEOUS POLARITY 
DIRECTION OF WINDING STARTS INSIDE ALL FOUR CORES 
INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL*D“70327 

SET LEADS EQUALLY SPACED AROUND PERIPHERTY 
OF WINDING* ORDER OPTIONAL 
WIPE IMPREGNATION DURING CURE CYCLE 
► PREHEAT WINDING AND IMPREGNANT TO 250°F 
IMPREGNATE WINDING WITH IMPREGNANT . 

PULL NO VACUUM 
BAKE 24 HRS AT I80°F 

, THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE ^ 

LESS THAN 10 MEGOHMS WHEN MEASURED AT 250VDC AFTER BAKING 

. BEF0R ^ l p N E D ^’ URE cycle CORES FOR a MINIMUM OF 5 DAYS PER ND-1002209 
CORES MUST MEET PERFORMANCE REQUIREMENTS OF SCO 1010688 AFTER 
TEMPERATURE CYCLING 



B 


LIST OF PARTS AND MATERIALS 


-HTT- 

INSTRUM ENT ATION 
LABORATORY 
Cawwidok. Maw. 


1000284 


USED ON 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


CORE a COIL 
ASSEMBLY 

(REACTOR . 
SECOND stage; 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001540 


SHEET 


I Of | 


L 


1001540 e> 









*■* pr. 


in .. 




P 

m 


t 

!■ 


WINDING DATA 


TOTAL NUMBER WINDINGS 5 


WINDING turns AWG , TYPE 0F 
NO. 'URNS W1RE S1?E W|N0 | NG 


RANDOM 


RANDOM 


RANDOM 

COMMON 


RANDOM 

COMMON 


RANDOM 

COMMON 



WINDING 

RESISTANCE 


IDENTIFICATION 


START I FINISH 



C-b <<*-!> 


ZONE SYM 


DESCRIPTION 


DATE I APPROVAL 






NOTES: 

1. INSULATE BETWEEN WINDINGS NO.I 8 NO.2 WITH A .005 POLYESTER 
WASHER -JO gj? PER MIL-I-G3I TYPE G 

2. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

3 . TURNS OR TURNS RATIO TOLERANCE tl% 

4. CORES MUST BE MATCHED QUAD AND TWO PART NO. 1001540 BE MADE 

5. («)0EN0TES THE SAME INSTANTANEOUS POLARITY 


SEE NOTE 5- 


SCHEMATIC 


9QWDG 590 


7 OWDG 4o 8 

KLJ 


• ■- 




.5 OWDG 396 


CORE r 


OWDG 192 3OWDG 204 


CORE 2 


___J 

( MS5-1L 


.460 DIA 
MAX 




y ! !; . A/R POLLYESTER 
I II ' A/R WIRE 
IJ! I _2_^2£E- 


| I QTY. 

1 IREQO. 


NOMENCLATURE 
OR DESCRIPTION 


1006711-22 _ 

1010688-1 

BEI^IMNO. *K»K*TW. 


' seeNOTE I 3 
' SEE DATA 2. 
' SEE NOTE 4 I 

MATERIAL FIND 
OR NOTES NO. 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARC M INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANQLES 


DO NOT SCALE THIS DNAWINS 


_ 1000284 

NEXT ASSY USED ON 

APPLICATION 


MIT 

IMBYIIO MENTATION LAS 

ComihaCT 


phwww 1 X. j iS-AS-gj 

MSC 

Wth/fL MTKOVAL I Mil 


LIST OF FARTS AND MATERIALS 

CORE G COIL 
ASSEMBLY 

Y REACTOR ~r ~“ 
SECOND stage; 
scale UmTn-TwSrm*: 

NONE —— - 


INSTRUMENTATION 

LASCftATO*Y 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

100540 








































































«r 


NOTICE — WHEN •OVCRNNINT DR*WINES. SPECIFICATIONS. OR OTHER OAT* 
ARE USED FOR ANT PURPOSE OTHER THAN IN CONNECTION WITH A DEFINITELY 
RELATED GOVERNMENT PROCUREMENT OPERATION. THE UNITED STATES GOVERN¬ 
MENT THEREDT INCURS NO RESPONSISILITT NOR ANT OSLISATION WHATSOEVER; 
AND THE FACT THAT THE SOVERNNENT MAY HAVE FORMULATED. FURNISHED. OR 
IN ANT WAT SUPPLIED THE SAIO DRAWINSS. SPECIFICATIONS OR OTHER DATA IS 
ROT TO RE RES ADDED ST IMPLICATION OR OTHERWISE AS IN ANT MANNER 
LICENSINC THE HOLDER OR ANT OTHER PERSON OR CORPORATION. OR CONVET- 
INS ARY RIRHTS OR PERMISSION TO MANUFACTURE. USE. OR SELL ARY 
FATE. 'EM INVENTION THAT HAT IN ARY WAY DC RELATED THERETO. 


± 






E 




5 


| REVISIONS 1 

I 

SYM 

DESCRIPTION 

DATE 

APPROVAL. 

1 

A 

etf/sso pee r-o#4. orifi 

tt/ufa 


1 



notes: 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL*D* 70327 

2. UNLESS OTHERWISE INDICATED ; 

' j ALL RESISTOR VALUES ARE IN OHMS. 

ALL CAPACITOR VALUES ARE IN UF. 

3* SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN 
! ACCORDANCE WITH MIL-STD‘440, 

WITH SN60WARP2 SOLDER PER QQ-S'571 


1 

DIODE 

1010286*2 

IN958 8 

400 MW 

12 

8 

♦ 

1010497 

500 PI V 

3.4 W 

II 

2 

CAPACITOR 

1006755-19 

3.3 

15V 

10 

1 

♦ 

1006755*69 

1.0 

35V 

9 

1 

RESISTOR 

1010695-91 

432 

1/8 W 

8 

1 



1010695-58 

196 

1/8 W 

7 

1 



1010694-143 

I.5K 

I/IOW 

6 

1 



1010694-67 

243 

i/iow 

5 

2 



1010694-96 

487 

I/IOW 

4 

2 



1010694-126 

IK 

I/IOW 

3 

1 

1 


1010694-302 

68.IK 

I/IOW | 

2 

1 

BOARD, PRINTED CIRCUIT 

1001542 



1 

QTY 

REQD 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO 

SPECIFICATION 

MATERIAL 
OR NOTES 

FIND 

NO. 



ft 















1000285 

NEXT ASSY 

USED ON 

| APPLICATION | 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 
FRACTIONS DECIMALS ANGLES 
■± ± ± 

t- - ' 

DO NOT SCALE THIS DRAWING 


MATERIAL 


HEAT TREATMENT 


FINAL FINISH 




t 


LIST OF MATERIALS 


M I T 

INSTRUMENTATION LAB 


DRAWN yT. / V. 
CHECKED 
APPROVAL^ 
APPROVAL — 


DATE ’*-* 1 **! 






71K L-4 


NASA APPROVAL 


MIT APPROVAL 



.MANNED SPACECRAFT CENTER 

* • HOUSTON, TEXAS 


PRINTED CIRCUIT BOARD 
ASSEMBLY 


CODE IDENT NO. 


INCHES 

I ■ l ■ I » .1 ,j_ 


nr 


SCALE NONE 

r~~ 


SIZE 


WT 


NASA DRAWING NO. 

/ 00 / 54 / 

| SHEET | OF |~ 




0 I * « 

PHOTOQRAPHWf SCALE ONLY j| 


ili • 

























3 


m r 






















































































_ REVISIONS 

DESCRIPTION 


A eey/s£.o P£* t-ojsp. Q5~3f/ 

HT REV/StO PER TDRR //660 
C REI//SLD PCR TORR 20757 


DATE ~ APPROVAL 

tt/it/a k/)l 

'\ L i 



AR 3IUC0NE RUBBER 
I DIODE 


CAPACITOR 


RESISTOR 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL“D-70327 

2. UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS. 

ALL CAPACITOR VALUES ARE IN UF. 

3. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN 
ACCORDANCE WITH MIL'S-6872. 

WITH SN60WRAP2 SOLDER PER QQ-S'571. 

4. COAT ASSEMBLY' WITH SILICONE RUBBER ; PART NO. I0I0649,WHEN COMPLETE, 



1010286-2 

IN958 B 

400 MW 


1010497 

500 PIV 

3.4 W 

MM 

mem 

1006755- 19 

3. 

3 

15V 

1006755-69 

1.' 

0 

35V 

1010695-91 

432 

I/8W 

8 

1010695-58 

196 

1/8 W 

7 

1010694-143 

I.5K 

I/IOW 

6 

1010694-67 

1_ — 

\l _ 

I/IOW 

IB 

B 

B 

1010694*96 

487 

I/IOW 

1010694-126 

IK 

I/IOW 

1010694-302 

68 

UK 

I/IOW 

2 


BOARD, PRINTED CIRCUIT 


NOMENCLATURE 
OR DESCRIPTION 


1001542 


SPECIFICATION 


MATERIAL 
OR NOTES 



UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 
FRACTIONS DECIMALS / 


M I T 

INSTRUMENTATION LAB 
Cammiooc. Mam. 


DO NOT SCALE THIS DRAWING 
MATERIAL 


PWS HO. COHTHACT 

ANGLES drawn ^ V-S- DATE 
“ CHECKED / r *'*.*2. 

' APPROVAL."^ 

APPROVAL. 


LIST OF MATERIALS _ 


MANNED SPACLlRAFT CENTER 

HOUSTON. TEXAS 


PRINTED CIRCUIT BOARD 
ASSEMBLY . 


1 000285 I00P285 

NEXT ASSY USED ON 

APPLICATION 


I HEAT TREATMENT 


CODE IDENT NO. SIZE 


C 


SCALE NONE |WT - 


NASA DRAWING NO. 

700/54/ 


[SHEET 1 OF t 


1 


3 


















































































































































































NOTES 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS. 

ALL CAPACITOR VALUES ARE IN UF. 

3. USE SOLDER SN60 PER QQ-S-571 

4. RI4 TO BE SELECTED PER ATPI0002&5 RANGE OF VALUES 
FROM I OHM THRU 10 OHMS PER PART * 1010604. 


REF 

DES 

PART NO. 

DESCRIPTION 

VALUE 

TOL 

RATING 

Rl 

1010311-302 

RESISTOR 

68 .IK 

±1% 

I/IOW 

R3 

1010363-786 



604 K .; 



1/4 W 

R4 

10103(1-126 



IK 



i/row 

R5 

10103 il — 96 



487 





R8 

1010311-96 



487 





R9 

1010311-126 , 



IK 





Rtl 

10103*1— 67 



487 




.. „ 

R12 

1010311-143 



1.5 K 




_ 

RI4 

1010604 



SEE N0TE4 



IW 

RI5 

1010364-1(6 



196 



I/8W 

RI6 

1010364-182 



432 



I/8W 

C2 

10(0393-029 

CAPACITOR 

1.0 

±10% 

35V 

C3 

1010393 

CAPACITOR 

3.3 



15V 

C4 

1010393 

CAPACITOR 

3.3 

1 


15V 

CR3 

1010497 

DIODE 

UTR52 


3.4 W 

CR4 








— 


CR5 








_ 


CR6 










CRIO 










CRII 










CRI2 










CRI3 






> 


3 


CRI4 

1010372-15 



H28544 

5% 

250 MW 

1 _ 

.1001542 

t/wr C*r BOARD 





































































f*J | ZONE SYM _ DESCRIPTION _ I P*TE I 

A REVISED PER TDRR 0S3S 2- Ut/u/ti 


DATE r APPROVAL 



TYPICAL TERMINAL AREA 
SEE NOTE 2 


JL, 


X 45° ±5° 
2 PLACES 


E 


NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. BOARD CONTAINS (45).042 DIA HOLES. AS SHOWN ON PRINTED CIRCUIT PATTERN 

3. ETCH PATTERN ON BOARD IN ACCORDANCE WITH PATTERN 
DRAWING 1001538. 

4. APOLLO G8 N PART NO. 1001542 TO BE STAMPED ON SIDE OF BOARD OPPOSITE PRINTED CIRCUIT PER MIL-STD-130. 

5. PRINTED-CIRCUIT BOARD PER MIL-P-55II0. 

6. MATERIAL: GLASS CLOTH-EPOXY RESIN LAMINATE FL-GE 03IC I/O PER 
MIL — p —13949 b. 

7. SOLDER COAT .0003 THICK MIN. USE SN60 WARP2 SOLDER PER QQ-S-571. 



A/R SOLDER _ 

I BOARD _ 

I PRINTED CIRCUIT PATTERN 


NOMENCLATURE 
OR DESCRIPTION 


1001538 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


' MOTE2f5 _ 

‘ SEE NOTE 2 \ 
REF _ 

MATERIAL FINC 
OR NOTES NO. 


1001541 11000285 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


SEE NOTE 6 


M I T 

IN S T R UMENTATION LAS 
CONTRACT 

NAS/0453 rOATE 


( DRAWN ]£. V. V. 
APPROVED FOR MSC 


LIST OP PARTS AND MATERIALS 

BOARD, 

PRINTED CIRCUIT 


QDDE IDENT. 


INSTRUMENTATION 

LABORATORY 
Canrripqr. Ma—. 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

1001542 




# ^ • INCHES = • j. 

I | • « • » » » » l 

& 0 I 2 

f A PHOTOGRAPHMfSCALE ORLY 


iroTsSff? 


























ts» * t 



n 


ZONE I SYM 


REVISIONS 

DESCRIPTION 


DATE I APPROVAL 



TYPICAL TERMINAL AREA 
SEE NOTE 2 


X 45° ±5° 
2 PLACES 


JL, 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. BOARD CONTAINS (45).042 DIA HOLES. AS SHOWN ON PRINTED CIRCUIT PATTERN 

3. ETCH PATTERN ON BOARD IN ACCORDANCE WITH PATTERN-- 

DRAWING 1001538. 

t . prPnted-c,'r?u,t eSiR 4 oS T E° s B M, L S - T ^ P 5 E 5 ?,o ON SIDE ° F BOARO refi “"--s™-' 30 - 

6LASS CL0TH -EPOXY RESIN LAMINATE FL-GE 03IC I/O PER 
MIL —P—13949 B. 

7. SOLDER COAT .0003 THICK MIN. USE SN60 SOLDER PER SPEC. QQ-S-571. 


A/R SOLDER _ 

I BOARD _ 

PRINTED CIRCUIT PATTERN 


NOMENCLATURE 
OR DESCRIPTION 


TERN 1001538 _ 

I IDENTIFYING* NO. SPECIFICATION 

LIST OF PARTS AND MATERIALS 


mote 2 is 

.SE E NOTE2 
REF 

MATERIAL 
OR NOTES 


_ 1000285 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: ~ 

SEE NOTE 6 


M IT 

INSTRUMENTATION LAI 

CONTRACT 

jys/yy ranr 

APPROVED 

CMCCRCO 

prawn ft* y. y, 

APPROVED FOR MSC 

/sJQ#/S. /n-y-L* 

iRIT/ll APPROVAL I DATE 


BOARD, 

PRINTED CIRCUIT 


CODE IDENT. 


INSTRUMENTATION 

LABORATORY 

Cam—ipm, Maw. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001542 

SHEET OF 
















































































B 


Li* * u .... 


MOTICS — WHIN «OVtNNNINT MUWINM. SPCCIPICAYIOWS. ON OYHIN »AYA 

M» W«D PWN AMY PYINH OTMID THAN IN CCANICTtON WITH A MFINmiY 

MLATtD MOVtNNNINY PNOCUMHINT OPINATION. TNI UNITID STATU MVSMN. 

HINT TNZMSY INCIIM NO NISPONSIIIUTV NON ANY OOUOATION WHATSOEVCNj 

AMO TNI TACT TNAT TNI DOVIRNNINT NAY NAVI POtNMLATIO. PWNNISNIO ON 

M ANY WAY MIPPIICD TNI SAIO DRAW I MSS. SPCCIPICATIONS ON ©THIN DAT IS 

NOT TO SC MOAROIO NY INPIICATION ON OTNIRWISI AS IN ANY NA««'*CN 

UCSNSINO TNI NOLMR OR ANY OTNIR PINSON OR CORPORATION. OR CONVIT- 

NM AM.’ RIRMTS OR PIRMISSION TO NANUPACTURt. MSI. OR SCU. AMT 
PATINTSS IRVCNTKM THAT NAY IN ANY WAY K RtLATBD TNCMTO. 


•YM 

oesemmoN 

I DATE 

i rrr*- 

A 

RCV/SCD r&t rox* 04&06 


LwL__ 


r 


1.000 i.005- 
PHOTO REF 
DIMENSION 


4 


Y APOLLO G a N SYSTEM \ 


l.000t.005 
PHOTO REF 
DIMENSION 


-.85 REF - 


PART NO. 


SERIAL NO. 


MFG NAME (REF) 



/ 
*- - OR 


MFG PART NO. 


.62 REF 


.06 R REF 


NOTES' 

i. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 
t .THERMOSETTING ADHESIVE ON BACK OF PLATE. 

3-DECAL TO MEET REQUIREMENTS OF MIL-P-6906. 

4.MARKINGS TO MEET REQUIREMENTS OF MIL-STD-130. 

i AND NDI0020I9 SHALL BE CLEAR AND LEGIBLE PER ND1002122 TYPE H CLASS I 
i ORIGINAL OF THIS DRAWING OR REPRODUCTION MADE BY PROCESS OR METHOD 
i SHALL INSURE DIMENSIONAL STABILITY 







1001614 . 


1000287 


100028$ 


1000285 


1000284 


1000283 

NEXT ASSY 

USED ON 

| APPLICATION | 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

± ± =fc 

DO NOT SCALE THIS DRAWING 


MATERIAL 

.008 ALUMINUM 


HEAT TREATMENT 


FINAL FINISH : BLACK ANODIZED 
BACKGROUND WITH CLEAR 
LETTERING_ 


QTY 

REQD 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


FIND 

NO. 


LIST OF MATERIALS 


M I T 

INSTRUMENTATION LAB 


DRAWN 

CHECKED 


DATE*3fl^ 

/-Jo-^3 



NASA 


APPROVAL 6JQ 


MIT APPROVAL 


MANNED SPACECRAFT CENTER 

HOUSTON. TEXAS 


PLATE - IDENTIFICATION 


CODE IDENT NO. 


SCALE 4/1 

r 


SIZE 


NASA DRAWING NO. 

1001543 


WT 


SHEET 


OF 


B 


^ INCHES 

I i I i ll I i I 

0 I 2 

PH OTOGRAPHKf SCALE ONLY 


1001543 |A| 

































1.000 ±.005> 
PHOTO REF 
DIMENSION 



-r 


l.000t.005 
PHOTO REF 
DIMENSION 





NOTES* 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. THERMOSETTING ADHESIVE ON BACK OF PLATE. 

3. DECAL TO MEET REQUIREMENTS OF MIL-P-6906. 

4. MARKINGS TO MEET REQUIREMENTS OF MIL-STD-130. 

AND NDI0020I9 SHALL BE CLEAR AND LEGIBLE PER ND1002122 TYPE E CLASS I 

5. ORIGINAL OF THIS DRAWING OR REPRODUCTION MADE BY PROCESS OR METHOD 
SHALL INSURE DIMENSIONAL STABILITY 






1001614 


1000287 


1000288 


1000285 


1000284 

• * * • «• » * 

• • * * * • • * • * 

• »«*•• • »« » * • 


IG00283 

NEXT ASSY 

USED ON 


APPLICATION 








































REDUCE 
4:1 TO 1.000 
±.005 


£1?QI00I 


REVISIONS 


DESCRIPTION 


DATE I APPROVAL 


Jm-REDUCE 4.1 TO 1.000 ±.005 H 



.62 REF 


PART RO. SER. SER.M0. 


OROER NO. 


.06 RADIUS REF 
4 PLACES 


NOTES* 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. THERMOSETTING ADHESIVE ON BACK OF PLATE. 

3. DECAL TO MEET REQUIREMENTS OF MiL-P-6906. 

4. MARKINGS TO MEET REQUIREMENTS OF MIL-STD-130. 


PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


1000287 

1000286 

1000265 

1000284 

1000283 


UNLESS OTHERWISE SPECIFIED INSTRUMEN 

DIMENSIONS ARE IN INCHES Cammhb 

TOLERANCES ON — *° 

FRACTIONS DECIMALS ANGLES DRAWN 

* * * CHECKED 

PQ NOT SCALE THIS DRAWING APPROVAL 

MATERIAL APPROVAL- 

.008 ALUMINUM 


M I T 

INSTRUMENTATION LAB 
Cammiiom. Mam. 


MANNED SPACECRAFT CENTER 


HOUSTON. TEXAS 


DATE 

, 7’3o~C3 


PLATE - IDENTIFICATION 


I HEAT TREATMENT 


I NASA APPROVAL (<J , 


I CODE IDENT NO.l SIZE 


NASA DRAWING NO. 




NEXT ASSY 


USED ON 


APPLICATION 


FINAL FINISH \ BLACK AN0DI1ED 
BACKGROUND WITH CLEAR 
LETTERING 


1001543 


MIT APPROVAL \ 


1 SCALE 4/1 







































































: d 


B 


t • 

T; 

n 

j&! 

tfkl 


i 




| REVISIONS /9-a 

77Z T - 1 

ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 


A 

REVISED PER TDRR 053 *6 


, uJli _ 



TYPICAL TERMINAL AREA 
SEE NOTE 2 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. BOARD CONTAINS (23) .042 DIA HOLES. AS SHOWN ON PRINTED CIRCUIT PATTERN 1001635. 

3. ETCH PATTERNON BOARD IN ACCORDANCE WITH PATTERN DRAWING 1001635. 

APOLLO GftN PART NO. 1001544 TO BE STAMPED ON SIDE OF BOARD OPPOSITE PRINTED CKT PER MIL-STD-130. 
5. PRINTED CIRCUIT BOARD PER MIL-P-55110. 

6.SOLDER COAT .0003 THICK MIN. USE SN60 WARP2 SOLDER PER QQ-S-571. 

7 MATD GLASS CLOTH-EPOKY RESIN LAMINATE FL-GE 03IC I/O PER MIL-P-13949B. 


1001626 


NEXT ASSY 


1000284 


APPLICATION 


-X '. 




UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


-SEE NOTE 7 


A/R 


QTY. 

REQO. 


SOLDER 


BOARD 


PRINTED CIRCUIT 


FATTERN 


NOMENCLATURE 
OR DESCRIPTION 


1001635 


PART OR 
IDENTIFYING NO. 


[SEE NOTE 6 


SEE NOTE 2 


SPECIFICATION 


REF 


MATERIAL 
OR NOTES 


FIND 

NO. 


LIST OF PARTS AND MATERIALS 


M I T 

INSTRUMENTATION LAB 
CONTRACT 


NAS 9A*3r5*Tf 


HE 




e.j.j. \8-to-€* 






Ju.a-jt-is 

flWIT/l^ APPROVAL DATE 


BOARD, 

PRINTED CIRCUIT 
(INDICATING BRIDGE^ 
V AMPLIFIER / 


SCALE 

4/1 


UNIT WT. 


CODE IDENT. 


- MIT- 

INSTRUMENTATION 

LABORATORY 

Camprio< 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001544 


SHEET | 


OF | 


in 

O 

o 


B 


INCHES : ; / 

I ‘ 1 ‘ I ■ 1 » ‘ 

0 12 
E - J PH OTOQRAPHKf SCALE ONLY 





















































notes: . 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. BOARD CONTAINS (23) .042 DIA HOLES. AS SHOWN ON PRINTED CIRCUIT PATTERN 100/635. 
a ETCH PATTERNON BOARD IN ACCORDANCE WITH PATTERN DRAWING 1001635. 

4. NASA DRAWING 1001544 TO BE CHANGED ON SIDE OF BOARD PER MIL-STD-130. 

5. PRINTED CIRCUIT BOARD PER MIL -P-55110. 

6. SOLDER COAT .0003 THICK MIN. USE SN60 SOLDER PER SPEC QQ-S-571. 

17 MATL-' GLASS CLOTH-EPOXY RESIN LAMINATE FL-GE 03IC I/O PER MIL-P-I394SB. 


A/R 

SOLDER 



SEE NOTE 6 

2 

1 

BOARD 



SEE NOTE 2 

1 


PRINTED 

CIRCUIT 

PATTERN 

1001635 


REF 


QTY. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IOCNTIFYINQ NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 


1 



UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 

TOl FRANCES 0* 



FRACTIONS DECIMALS ANQLES • 






00 NOT SCALE THIS DRAW!NO 


1000284 

MATERIAL: 

SEE NOTE 7, 

NEXT ASSY 

USED ON 

| APPLICATION 



LIST OF PARTS ANO MATERIALS 


M IT 

I NS T R UMENTATION LAB 
CONTRACT 


NAS 9,1*3 

ar“ 


m 


. DATf 




APPROVED TOR MSC 

I MIT/IL APPROVAL I Di 


Mit/i^ approval dati 


BOARD, 

PRINTED CIRCUIT 
/INDICATING BRIDGE) 
V AMPLIFIER / 


SCALE 

4/1 


UNIT WT. 


CODE I DENT. 


Wl I T 

INSTRUMENTATION 

Lm^unaTORY 
Cammuoor. Ma—. 


MANHCO 

SPACECRAFT CENTER 

HOUSTON TEXAS 


NASA DRAWING NO. 

1001544 


SHEET 


1 




















































































































OATS 


APPROVAL 


REVISIONS 

DESCRIPTION 


ZONE SYM _ DESCRIPTION _—f 

■ _ A REVISED PER FDRR 04529 


.812 REF —W 


.166 BSC 


-.203 BSC ' 
4 PLACES- r*'.!* 


t'.LAT” 


SEE NOTES 2 8 3 


.094 ±.01 


014 + 002 
j~ - OI9 -.003 


.13_T 

.11 

2 PLACES 


i_6_9_5_8_L 


! 10 7 4 3 2 


1.152 

1.136 


l33 + 002 0IA THRU 
^OifoiAl' 0 H ° LES 


notes: 

1. INTERPRET IN ACCORDANCE WITH MIL-0-70327. 

2. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

3. ENGRAVE OR METAL STAMP PER NDI0020I9 (.09 CHARACTERS). 

4 . FINISH-TIN PLATE PER MIL-T-10727 TYPE H (HOT OIP). 

5. BREAK ALL SHARP EDGES .010 MAX. 


COVER. SQUARE 


\MOM 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MIT 

i nstr umentation la* 

CONTRACT 


LIST OF PARTS AND MATERIALS 


COVER-MACHINED 


1000284 


INSTRUMENTATION 

laboratory 

Camsstops. Mass. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 


UNIT WT. 


CODE IDENT. 


1001546 


APPLICATION 





















































-.094 REF 

.019 REF^ 


r 

i 


D 


C 


notes: 

1. INTERPRET IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

3. ENGRAVE OR METAL STAMP PER NDI0020I9 AND ND-I002I22, TYPE It,CLASS I,.09CHARACTERS. 

4. FINISH-TIN PLATE PER MIL-T-10727 TYPE H (HOT DIP). 

5. BREAK ALL SHARP EDGES .010 MAX. 


4 


3 


1 

COVER, SQUARE 

1010691-5 



1 

QTY. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 


LIST OF PARTS AND MATERIALS 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 








DO NOT SCALE THIS DRAWING 

1001547 

1000284 

MATERIAL: 

NEXT ASSY 

USED ON 


| APPLICATION 




COVER, MACHINED 


SCALE 

2/1 


UNIT WT. 


CODE I DENT. 


M I T 

INSTRUMENTATION 

LABORATORY 

CAMWIPOi, MA—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 


1001546 


SHEET I 


OF | 





0 I 

PH OTOORAPHIlf SCALE ONLY 


B 


A 


1001546 






















































i 


& 




| REVISIONS 11 

ZONE 

SYM 

DESCRIPTION 1 DATE 1 

APPROVAL ■ 


A 

REVISED PER TDRR 0S3S& 

hjjL- 1 


©did® 


© © © @ © 

10 7 4 3 2 




•j040 MAX 


NOTES: 

1. INTERPRET IN ACCORDANCE WITH STANDARDS PRESCRIBED 
BY MIL—D—70327. 

2. SOLDERING PER MIL-S-6872A WITH SN50 WARP2 SOLDER 
PER QQ-S-571. 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 



rULlilH H 

FRACTIONS DECIMALS ANGLES 






DO NOT SCALE THIS DRAWING 


1000284 

MATERIAL: 

NEXT ASSY 

USED ON 


| APPLICATION 



f 


A/R SOLDER 


10 


QTY. 

REQO. 


TERMINAL 


COVER- MACHINED 


NOMENCLATURE 
OR DESCRIPTION 


/0/0690-/ 


1001546 


PART OR 
IDENTIFYING NO. 


[SEE NOTE 21 3 


SPECIFICATION 


MATERIAL 
OR NOTES 


FIND 

NO. 


LIST OF PARTS AND MATERIALS 


MIT 

INSTRUMENTATION LAS 


-&T7. 


"daTT . 


V-/3-63 


M4 



MSC 


M. 


IIT/IL APPROVAL 




r/ij. appi 




24J 


DATE 




COVER-ASSEMBLY 


SCALE 

2/1 


UNIT WT. 


L 


INCHES 

i I lull 




COOE IOENT. 


MiT 

INSTRUM ENTATtON 
LABORATORY 
Cammioos. Mam. 

/ 

OWR. NO. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWINQ NO. 

1001547 


SHEET I OF I 





0 1 

PH0T0GRAPHI<r9CALE ONLY jl 


: 



Fit A: 

Hkt. .V ft • 


i -• 


I 


S.K 




r-' 


i 


- : i 
- 


; i 


. * ft 


ft. I 


PI- 

h 4 


























































































! 


r 


I- 


■» : 


-1 


1 


I- 




r 


^■ir 


! i 
• I * 


i. F 


i 

J* .. 


i 

i: I 




I 


1 


<3 




REVISIONS 



ZONE 

SYM 

| DESCRIPTION 

I ■»« 1 

APPROVAL 


A 

[revised per tdrr 

05360 



SEE NOTE 3: 
2 PLACESTH 



SEE NOTE 2 


notes: 

•.INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. SURFACE TO BE FLAT WITHIN .015. T.I.R. 

3. BRAZE PER MIL -B-7883.WITH CLASS 4 SILVER SOLDER PER QQ-S-561. 

4 . FINISH — TIN PLATE PER MIL-T-10727 TYPE H (HOT DIP). 

5. PA.N HEAD SCREW ,CRES, 4 *40 NC- 2Aw. X 5/lG LS PER MS35E3VI4- 





Cfl 


'if 

pW' "W - 


*- vlr[ 


pr* 

$- 


‘ ■>! 

: : !: . . 

I 

■ r 


■ f 

■ 




■ I 






7* 

it.-- 


? - 

: : -. iM- 




h * 


1*^' :a ! : 
















REVISIONS 


ZONE I SYM 


DESCRIPTION 


; SEE WOT E 3: 

: z places' -: 




SEE NOTE 2 


NOTES: 


1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. SURFACE TO BE FLAT WITHIN .015. XI.R. . 

3. BRAZE PER MIL-B-7883. 

4. FINISH —TIN PLATE PER MIL-T-10727 TYPE 31 (HOT DIP). 

5. PAN EIEAD SCREW.CRES, 4-40 NC-2A. X LG PER MS35ES3.-14 


CASE-MACHINED 
SCREW _ 

NOMENCLATURE 
OR DESCRIPTION 


11001545 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


SEE NOTE 5 

MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS D EC I MALS ANQLES 


DO NOT SCALE THIS DRAWING 


MIT 

INSTRUMENTATION Ul 

CONTRACT 


1000284 


LIST OF PARTS AND MATERIALS 


CASE - ASSEMBLY 


COOC IOENT. 


INSTRUM ENTATIOM 
LABORATORY 
Camhidw, Maw. 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 


1001548 


/miCATION 


3 





















































REVISIONS 


g j i fr -5. 


ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 


A 

REVISED PER TDRR 0536/ 


-UliL — 


WINDING DATA 


TOTAL NUMBER WINDINGS 4 


WINDING 

NO. 

TURNS 

TAP 

AT 

AWG WIRE SIZE 

TYPE OF 
WINDING 

' 1 

LEADS 

WINDING 

RESISTANCE (REF) 
OHMS ± 20% (a) 25°C 

LENGTH 

SIZE 

” IDENTIFICATION 

START 

TAP 

FINISH 

PRI 

600 


41ZZ__ 

RANDOM 

6" 

30 

I 

. _ 

- z 

39 

SECI 

200 

100 

* : 4i: : 

RANDOM 

6" 

30 

. 3 

4 

5 _ 

14.5 

SEC 2 

700 

350 

Z 41 Z 

RANDOM 

6" 

30 

” €> 

7 

8 

50 

SEC 3 

600 

300 

z 4i 

RANDOM 

6" 

30 

~9 

io 

\\ _ 

47 


notes: 

L (■) DENOTES THE SAME. INSTANTANEOUS POLARITY. . 

2. PREHEAT WINDING AND IMPREGNANT TO 250°F IMPREGNATE WINDING 

WITH IMPREGNANT. PULL NO VACUUM. BAKE 24 HRS AT I80°F. _ 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE ± 1%. 

. G. 77/C RESlSTAfi/£ BCTH/EErf H/lf/o/Z/GS SHALL t/or BE LESS T/Ja/Z 
(OMEGOf/MS Wf/Erf MEASURED AT 250 VDC AFTER BAKING 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED 
BY MIL-D-70327. 

8. BEFORE WINDING TEMPERATURE CYCLE CORES FOR A MINIMUM OF 
5 DAYS- PER ND —1002209 CORE MUST MEET PERFORMANCE 
REQUIREMENTS OF SCO 1010689 AFTER TEMPERATURE CYCLING. 


SEE 





UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 



FRACTIONS DECIMALS ANGLES 






DO NOT SCALE THIS DRAWING 


1000284 

MATERIAL: 

NEXT ASSY 

USED ON 


| APPLICATION 



A/R 


A/R 


A/R 


QTY. 

REQD. 


IMPREGNANT 


WIRE (LEAPsV 


WIRE. 


CORE 


NOMENCLATURE 
OR DESCRIPTION 


IOiO<2>87*-l 


I 00 & 7 U-I 3 


iooG 7 i\-aa 


I010G8VI 


PART OR 
IDENTIFYING NO. 


AWG 30 


AWG 41 


SPECIFICATION 


NOTE 2*4 


SEE DATA 


SEE DATA 


MATERIAL 
OR NOTES 


FIND 

NO. 


LIST OF PARTS AND MATERIALS 


MIT 

INSTRUMENTATIOfl 

COM TRACT 

LAS 

"5STT 

APPROVtO jKA/iiUji: 


CHECKED /&, /C 


DRAWN | E. V# V. 

3S3-63 

approved por MSC 

l£f/f APPROVAL 

DATE 




CORE / COIL 
ASSEMBLY 

(TRANSFORMER, POWER) 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


-RTTT- 

INSTRUMENTATION 

LABORATORY 
Cam—ipm, KUm. 


SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWINQ HO. 

1001549 


SHEET I 


OF | 


INCHES 


0 I 

PHOTOGRAPHUfSCALE ONLY 


1 


i 





























WINDING DATA 


WINDING 

NO, 

TURNS 

TAP 

AT 

AWG WIRE SIZE 

TYPE OF 
WINDING 

LEADS 

TOTAL WINDING 
RESISTANCE (REF) 
OHMS ± 20% (a) 25°C 

LENGTH 

SIZE 

IDENTIFICATION 

ST ART 

TAP 

FINISH 

PRI 

600 


41 

RANDOM 

6“ 

30 

1 


2 1 

39 

SECI 

200 

100 

41 

RANDOM 

6“ 

30 

S 

4 

5 

14.5 

SEC 2 

700 

350 

41 

RANDOM 

6" 

30 


7 

8 

50 

SEC 3 

600 

300 

41 

RANDOM 

6“ 

30 

* 

\o 

U 

47 


notes: 

1. {■) DENOTES THE S/aWIF. IU'oTKNTA.NEOUS POLAvRITY 

2. PREHEAT WINDING AND IMPREGNANT TO 250°F IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24 HPS AT I80°F. 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE ± 1%. 

G. ThtC RES/STAa/E BETH/EEt/ iRltJo/FGS St!ALL tJoT BE LESS THAt! 
tO MEGOHMS WFEtJ MEASURED AT'EEOVDC AFTER BAKING 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED 
BY MIL - D-70327. 

8. BEFORE WINDING TEMPERATURE CYCLE CORES FOR A MINIMUM OF 
5 DAYS PER ND — 1002209 CORE MUST MEET PERFORMANCE 
REQUIREMENTS OF SCO 1010689 AFTER TEMPERATURE CYCLING. 


REVISIONS 


SYM 


B 


DESCRIPTION 


RE VISED PER TD R R 05 b& > / 

REVISED PER TDRR H665 




APPROVAL 




SCHEMATIC 


“I. 


SEE t/0TE / 


SEC I 
3 4 5 



SEC 2 
6 7 8 





n 


SEC 3 
9 10 II 


-I 


“T 

.48 DIA 
MAX 

_1_ 


.30 

MAX 


B 


A/R 

IMPREGNANT 

ioiocbaT-1 


NOTE £ 14 

4 

A/R~ 

WIRE (LEA.DE)) 

100G71M3 

AWG 30 

5EE DATA 

s 

A/R 

NNIR^ 

IOOG7l\-££ 

AWG 41 

SEE DATA 

2. 

1 

COPE 

10100.8*3-1 



1 

OTY. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 





UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 



FRACTIONS DECIMALS ANGLES 






DO NOT SCALE THIS DRAWING 


1000284 

MATERIAL* 

NEXT ASSY 

USED ON 


| APPLICATION 


—-1 , 


LIST OF PARTS AND MATERIALS 


M I T 

INSTRUMENTATION LAS 

CONTRACT 

^IW 


&7C- 


ev.v. 




CORE / COIL 
ASSEMBLY 

(TRANSFORMER, POWER) 


-MIT ” 

INSTRUMENTATION 

LABORATORY 

OWMIOW, MA—. 


te-/3 63\ 


APPROVED FOR MSC 

/,)q/2lL /o-2-6 

MfT/IL APPROVAL 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

D0I549 


I SHEET I 


OF I 


1001549 
















WINDING DATA 


TOTAL NUMBER WINDINGS 4 


WINDING 

NO. 

TURNS 

TAP 

AT 

AW& W\HE SIZE 

TYPE OF 
WINDING 

LENGTH 

SIZE 

LEADS 

IDENT\nCATlON 
STAR T| TAP FINISH 

PRI 

600 


Z4i :z :_ 

RANDOM 

6* 

30 

: i 

.. z 

SECI 

200 

100 

z;4i: z 

RANDOM 

6" 

30 

3 

A 5 ... 

SEC 2 

700 

350 

z*r z 

RANDOM 

6" 

30 

€> 

7 8 

SEC 3 

600 

300 

Z4i 

RANDOM 

6" 

30 

“9: 

lO II 


notes: 

1. (■) DENOTES THE SAME. INSTANTANEOUS POLARITY 

2. PREHEAT WINDING AND HYSOL TO 2.50° F IMPREGNATE WINDING 

WITH HYSOL. PULL. NO VACUUM. BAKE E4 HRS AT 180° F - 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE ±1%. 

6. TtjC RESISTAfi/C SETV/EE// H/lrfo/ftG St!ALL tJor BE LESS T/Ja*I 
_ tO MEGOHMS M/UEjJ MEASURED AT 500 VDC AETCX BAKING 



f/0TE / 


SEC I 
3 4 5 




SCHEMATIC 

SEC 2 
6 7 8 

ID 

n 

I 2 
PR I 


SEC 3 
9 10 II 

ID 


-1 

.3° | 

MAX . 


.48 DIA 
MAX 


A/R HYSOL 


IOIOC.&7 -1 _::::::::: 

NOTE £(4 

4 

A/R WIRE ( 

LEADS) 

I00G7U-13 

SEE DATA 

B 

A/R WIRE. 

. ; .. 

_ !OOG7i\-a2 : _:. 

^>EE DATA 

Z 

1 CORE. 


I010C83~I 


\ 

QTY. 

NOMENCLATURE 

PART OR SPECIFICATION 

MATERIAL 

FINO 

REQO. 

OR DESCRIPTION 

IDENTIFYING NO. wtwriwumw 

OR NOTES 

NO. 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS OECtMALS ANGLES 


DO NOT SCALE THIS ORAWINS 

1000284 MATERIAL: 

NEXT ASSY USED ON 

APPLICATION 


MIT 

IN STR UMENTATION LAD 

CONTMCT 


LIST Of PARTS AND MATERIALS 

CORE ^ COIL 
ASSEMBLY 

(TRANSFORMER POWER) 


IW9Tm»HeWTATK>H 

LABORATORY 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA ORAWINS NO. 


CODE IDENT. 


I00!549 

SHEET OF 



































































A 


3 


2 


1 


/ 


TOTAL NUMBER WINDINGS 9 


WINDING DATA 


& 


ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 


A 

[REVISED PER TDRR 053&Z 


JJBH 


WINDING 

NO. 

TURNS 

AWG WIRE 
SIZE 

TYPE OF 
WINDING 

WINE 

RESIST 

)ING 

Leads1 

ANCI 

LENGTH 

SIZE 

IDENTIFICATION I 

UHMb TdU'Jotaj 

25°C(REF)^ 

START 

FINISH 

1 

250 

41 

RANDOM 

13 

6" 

AWG 

30 

1 

2 

2 













3 

4 

3 













5 

6 

4 

i 

_ 



y 


y 

f 





7 

8 

5 

200 

, r ■ 

■' - • 

RANDOM 
COMMON 
TO CORES 
182 

17 



- 


9 

10 

6 

\ 




RANDOM 
COMMON 
TO CORES 
3 8 4 







II 

12 

7 

550 



RANDOM 
COMMON 
BIFILAR 
TO CORES 
1,2,3,84 

94 





13 

14 

8 




1 

RANDOM 
COMMON 
BIFILAR 
TO CORES 
1,2,3,8 4 

1 

* ' 




■ 

15 

16 

V 

9 

■ V 

200 



RANDOM 
COMMON 
TO CORES 
1,2,3, 8 4 

36 





17 

18 


r 


1 


SCHEMATIC DIAGRAM 



notes: 

1. 

2 . 

3. 

4. 

5. 

6 . 

7. 

e. 


9. 

10 . 

11. 

12 . 

13. 


INSULATE BETWEEN WINDINGS NO. 1,2,3,84 WITH A .005 POLYESTER WASHER $9 ?J?' 
PER MIL-I-631 TYPE G. ^ . 

(■> DENOTES THE SAME INSTANTANEOUS POLARITY. 

CORES MUST BE MATCHED QUAD. 

WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

TURNS OR TURNS RATIO TOLERANCE ±1%. 

DIRECTION OF WINDING STARTS INSIDE ALL FOUR CORES. 

INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 
MEASURE THE RESISTANCE OF THE TWO CONTROL WINDINGS (13 TO 14 8 15 TO 16). ADD 
SUFFICIENT LENGTH OF # 41AWG WIRE (PART NO. 1006711-22),TO EACH WINDING, TO 
PROVIDE A DC RESISTANCE OF 154 ±2% OHMS PER CONTROL WINDING. MATCH WINDING 
RESISTANCES TO .tOHMS (® 75°F. ATTACH LEAD PER NOTE 9 AND TABULATE. 

SET LEADS EQUALLY SPACED AROUND PERIPHERY OF WINDING. ORDER OPTIONAL. 

WIPE IMPREGNATION DURING CURE CYCLE. ’ 

PREHEAT WINDING 8 IMPREGNANT TO 250°F. IMPREGNATE WINDING WITH IMPREGNANT. 
PULL NO VACUUM. BAKE 24 HRS AT I80°F. 

THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS WHEN 
MEASURED AT 250 VDC AFTER BAKING. 

BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A MINIMUM OF 5 DAYS PER 
ND-1002209. CORES MUST MEET PEFORMANCE REQUIREMENTS OF SCD 1010688 
AFTER TEMPERATURE CYCLING. 




L_____ 




A/R 

WIRE(LEADS) 

1006711-13 

AWG 30 

SEE DATA 

5 

A/R 

IMPREGNANT 

1010687-1 


SEE NOTE Will 

4 

A/R 

POLYESTER 



SEE NOTE 1 

3 

A/R 

WIRE 

1006711-22 

AWG 41 

SEE DATA 

2 

4 

CORE 

1010688- 2 


SEE NOTE 3 

1 

<?ty. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 


1000284 


APPUCAHOH 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 
FRACTIONS 


DO NOT SCALE THIS DRAWING 


LIST OF PARTS AND MATERIALS 


MIT 

MCNTATI 

CONTRACT 


mm 




TOT 






V3-/4-63 


ANMNB FOR MSC 


MMT/IL AFP R OVA 


SKt/JL APPROVI 


AJL 


DATE 


CORE J^COIL ASSY 

(REACTOR - ' 
FIRST STAGE) 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


M IT 

INSTRUMENTATIOM 

LABORATORY 
Cammim 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001550 


SHEET | 


OF | 


INCHES 

i 1 i.ui.L 


0 I 

PHOTOGRAPHICf SCALE ONLY 




















1 


L 


1 


WINDING DATA 


TOTAL NUMBER WINDINGS 9 


WINDING 

NO. 

TURNS 


TYPE OF 
WINDING 

WINDING 
RESISTANCE- 
OHMS ±20% (a) 
25°C(REF) ^ 

EXCEPT AS NOTED 

LEADS 

LENGTH 

SI2 


■11 liHIII Hil 111 

E 

START 

FINISH 

1 


4T^ 

RANDOM 

13 

6“ 

AWG 

30 

1 

2 

2 

■i 

■n 











3 

4 

3 













5 

6 

4 







1 

p 





7 

8 

5 

200 

i ■ 

* .. ■■ 

RANDOM 
COMMON 
TO CORES 
182 

17 



1 

i 

9 

' 10 

6 

i 

1 

■ 

u 

RANDOM 
COMMON 
TO CORES 
3 8 4 


■ 



1 

i 

n 

12 

7 

550 



RANDOM 
COMMON 
BIFILAR 
TO CORES 
1,2,3,84 

85.3 ±10% 
SEE NOTE 8 



1 

l 

m 

BB 

8 

1 

1 

| 

1 

RANDOM 
COMMON 
BIFILAR 
TO CORES 
1,2,3,8 4 

■ 

■ 



1 

l 

H 

81 

■ V r 

9 

* \t 

200 

■ 

■ 

BH 

36 



1 

i 

17 

* 18 



REVISIONS | 

l 

ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 



A 

REVISED PER TDRR OS3&Z 


iJil 


B 

REVISED PER TDRR 06065 

>-3HcA- 




w'' 

--■- -J 



NOTES: do nn 

I. INSULATE BETWEEN WINDINGS NO. 1,2,3,84 WITH A .005 POLYESTER WASHER 
PER MIL-I-631 TYPE G. .ct \.u. 

*.(■) DENOTES THE SAME INSTANTANEOUS POLARITY. 

3. CORES MUST BE MATCHED QUAD. 

4. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

5. TURNS OR TURNS RATIO TOLERANCE ±1%. 

6. DIRECTION OF WINDING STARTS INSIDE ALL FOUR CORES. 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 


9. SET LEADS EQUALLY SPACED AROUND PERIPHERY OF WINDING. ORDER OPTIONAL. 

10. WIPE IMPREGNATION DURING CURE CYCLE. ’ 

11. PREHEAT WINDING 8 IMPREGNANT TO 250°F. IMPREGNATE WINDING WITH IMPREGNANT. 
PULL NO VACUUM. BAKE 24 HRS AT I80°F. 

12. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS WHEN 
MEASURED AT 250 VDC AFTER BAKING. 

13. BEF0RE WINDING, TEMPERATURE CYCLE CORES FOR A MINIMUM OF 5 DAYS PER 
ND-1002209. CORES MUST MEET PEFORMANCE REQUIREMENTS OF SCD 1010688 
AFTER TEMPERATURE CYCLING. 

8.ADD SUFFICIENT LENGTH OF #41 WIRE (PART NO. 1006711-22), TO EACH CONTROL 
WINDING TO PROVIDE ATOTAL DC RESISTANCE INCLUDING Rl 8 R2(PART NO.1010694-II), 
OF I54±2% OHMS AT 77°F PER CONTROL WINDING. IN ADDITION MATCH THE TOTAL ' 
CONTROL WINDING RESISTANCES TO WITHIN 0.1 OHM AT 77°F AND TABULATE, 

ATTACH #41 AWG WINDING WIRE TO RESISTOR AND USE #30AWG WIRE (1006711-13) 
ATTACHED TO THE RESISTORS FOR LEADS 14 8 16. 


I 

I 

I 

I 




_J. 


2 

RESISTOR 

1010694-11 

63.4 I/IOW 

SEE NOTE 8 

CE 

A/R 

WIRE(LEADS) 

1006711-13 

AWG 30 

SEE DATA 

nr 

A/R 

IMPREGNANT 

I0I0687-L 


SEE NOTE Mil 

4 

A/R 

POLYESTER 



SEE NOTE 1 

3 

A/R 

WIRE 

1006711-22 

AWG 41 

SEE DATA 

2 

4 

CORE 

1010688- 2 


SEE NOTE 3 

1 

QTY. 

RCQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

material 

OR NOTES 

FI NO 
NO. 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 



FRACTIONS DECIMALS ANSI El 






DO NOT SCALE THIS DRAWING 


1000284 

MATERIAL: 

NEXT ASSY 

USED ON 



M I T 


rmt 




/P.7.V. 


m 


\ 3-/+-63 


6JZ./QL 

MT/IL APPI 


MSC 


Mu/)L APPROVAI 

vi£*£z m 


DATE 


wm 


LIST OF PARTS AND MATERIALS 


CORE ^COIL ASSY 

(REACTOR 

FIRST STAGE) 

-MfT 

INSTRUMENTATION 

LABORATORY 
cammiomc. mam. 

dim no. 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 

NASA DRAWING NO. 

001550 

SCALE UNIT WT. CODE IDENT. 

NONE , -- - 

_ —. 

SHCETI OF | 


APPLICATION 










































































WINDING DATA 


( „ 1 Aiil I. , ( . 

TOTAL NUMBER WINDINGS 6 


WINDING turn* awg WIRE 
No TURNS S IZE. 



TYPE OF 
WINDING 


RANDOM 


RANDOM 


RANDOM 

COMMON 

RANDOM 

COMMON 


RANDOM 

COMMON 


RANDOM 

COMMON 


WINDING 
RESISTANCE IlENGThI SIZE 


IDENTIFICATION 


START I FINISH 



notes: 

1. INSULATE BETWEEN WINDINGS NO.) a NO.2 WITH A .005 POLYESTER 

WASHER ^ PER MIL-1-631 TYPE G.- 

2. (a) DENOTES THE SAME INSTANTANEOUS POLARITY. 

3. CORES MUST BE A MATCHED QUAD 8 TWO PART N0.I00I550 BE MADE. - 

4. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

" 5.TURNS OR TURNS RATIO TOLERANCE ±1%. 


SEE NOTE 2 


SCHEMATIC 


lloWDG 6oI2 


90WDG 5010 


T 0 S 


5oWDG 3p6 


CORE r 


.CORE 2 


loWDG 162 36WDG 264 


|-- 



''' •» ' '' * 


.480 DIA 
MAX 


•I I |l> M 

lb 'Hi: >i 




UNLESS OTHERWISE SPCCtFlED 

DIMENSIONS ARE IN INCHKB 
TOLERANCES ON 

FRACTIONS DECIMALS ANQLES 


DO NOT SCALE THIS DRAW1NQ 


1000284 


ZONE I SYM 


REVISIONS 

DESCRIPTION 




DATE I APPROVAL 


n 

I 


A/R POLYESTER 
A/R WIRE 
2 CORE 


NOMENCLATURE 
OR DESCRIPTION 


1006711-22 
1010688—i 

PART OR 
IDCNTIFYtNQ NO. 


SPECIFICATION 


SEE NOTE I 
SEE DATA 
SEE NOTE 3 

MATERIAL 
OR NOTES 


MIT 

I N trilW MgNTATIOR LAS 

CONTRACT 


I *7 -/ _ 

>KM MAC 


LIST Of PARTS AND MATERIALS 

CORE £ COIL ASSY 

(reactor - ‘ :: 

FIRST STAGE) _ 


INSTNUM CNT ATION 

LAouhaTORY 
CAatmiPOK. Ma—. 

wa 

MANNED _ 
SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWINQ NO. 


COOE IOENT. 


T/|L APPROVAL 


/OTUCATKW 


NONE 


1001550 


3 





















































































































































































view Y-Y 

SCALE M 

SHOWN wtthCD^RTiauy removeo 


NOTES: 

1. WTFRPRET DRAWJNG IN ACCORDANCE WITH MIL-0-70327 

2. ITEMS ( ~2~) < (5) ARE OPTIONAL, BUT WHEN USED THEY MUST BE ASSEMBLED BEFORE BRAZING 
AND MACHINED FLUSH WITHIN .001 MAX AFTER BRAZING 

3 . DIP BRAZE PER HD 1002073 EXCEPT AlR BLAST QUENCH TO ROOM TEMP PRIOR TO CLEANING 

4. HEAT TREAT PEP MIL-H-608S TO BRINELL 70 MIN HARDNESS TO BE CHECKED AT INDICATED 
AREAS ONLY 

A. SOLUTION HEAT TREAT AT 970*F ± IO*F FOR 2 HOURS ±5 MINUTES-AIR BLAST QUENCH 

B. AGE AT 350*F ±IO*F FOR 6 HOURS 15 MINUTES 

t. IDENTIFY USING DRAWING NO., REVISION LETTER 4 MANUFACTURERS SYMBOL PER NDI0O2O® 

6. HYDROSTATIC PROOF TEST HEAT EXCHANGER PASSAGES AND FITTINGS AT 9OPSIG.N0 LEAKAGE PERMISSIBLE 
7* CON CAL ‘SURFACE- $ THREADS MUST BE COATED WITH PROTECTIVE COMPOUND PRIOR TO 
'©RAZING OPERATION - CON CAL SURFACE £ THREADS MUST NOT BE DAMAGED DURING 
CLEANING OPERATION 

-PRESSURE TEST 06E USING HELIUM LEAK DETECTOR 
MAX ALLOWABLE LEAK RATE 1.0 * IO ‘ 5 CC/SEC OF HELIUM • I ATMOSPHERE PRESSURE DIFFERENTIAL 

9 _9-K —iP AT c/'HANGER rAsj-GES PER ATP .COCCC. 

10 ITEM 7 TC BE CUT TC LENGTH AT ASSEMBLY TC PROJECT ’NTO ITEM II, .125 MIN. 


THIS AREA TO BE 

COMPLETELY FILLED 



SECTION J-J 

SCALE 1 2/l 
6 PLACES 


l7 Jf11 Tm sp 








































































































8 


a. j 

o\ 


f) 





2 PLACES 


view Y-Y 

s: \lE i i 

5ho m wrm(l[)nARTiAu>i re moved 


NOTES: 

L WTETRPRCT orating IN ACCORDANCE WITH mil-0-70327 

2. ITEMS CT} < (T'! ARE OPTIONAL, BUT WHEN USED THEY MUST BE ASSEMBLED BEFORE BRAZING 
AND MACHINED FLUSH WITm'N .001 MAX AFTfR BRAZING 

3. DIP BRAZE AND RADIOGRAPHICALLY INSPECT PER NDI00P073 EXCEPT AIR BLAST QUENCH 
TO ROOM TEMPERATURE PRIOR TO CLEANING. 

4. MEAT TnLAT F£G Mil-h-6086 TO BRINELL 70 MIN HARDNESS TO BE CHECKED AT INDICATED 
AREAS ONLY 

A. SOL' TION HEAT TREAT AT 970*F ± 10 # F FOR 2 HOURS -5 MINUTES — AIR BLAST QUENCH 

B. AGE AT 350*F±»0T FOR 6 HOURS t 5 Minutes 

IDENTIFY USING DRAWING NO., REVISION LETTER < MANUFACTURERS SYMBOL PER *0002019 

tot HYDROSTATIC PROOF TEST HEAT EXCHANGER PASSAGES AND FITTINGS AT ^K) PSIG. NO LEAKAGE PERMISSIBLE 
7. CON CAL SURFACE 5 THREADS MUST BE COATED WITH PROTECTIVE COMPOUND PRIOR TO 
BRAZING OPERATION - CON CAL SURFACE * THREADS MUST NOT BE DAMAGED DURING 
CLEANING OPERATION 
-PRESSURE TEST CASE USING HELIUM LEAK DC TEC TO* 

ma* allowable leak rate i.o ■ 10 ' 5 cc/sec of heuum • i atmosphere pressure differential 

9. UC.AK CntCK H: AT r /' HANf*r H 'A ,.,-^rS Phfi Air , v \ . , 

10. 'TEM 7 TO BE CUT TC LENGTH AT ASSEMBLY TC FRC JECT ’NTO ITEM ||, .125 MIN. 


n 

4 . ;* 

•ISS 

► -w .250 MAX 


SECTION J-J 
scale s 2/1 


























































: s r- 

































%«*.• .HBL 




























IGOICHB 





































































































■ox=r«ca| 




1001558 


































































6 




























































































7 


e 


5 





VIEW E-E 



section F-F 


cm 



5 


| 1001559 


[WE7 

A 





























MOUNX CONNECTOR 
: ASSEMBLY 


16X OUTER AXIS 













































































































1 


ZONE 


I ”■ I 


REVISIONS f)(p T-47 


DESCRIPTION 


DATE I APPROVAL 


2.00 





\ 



L :i& DIA 


ifz3 DIA thru 
C'SK tO* TO.750 DIA 


SEE NOTE 3 


‘ notes: -- --::' - : v: ...it - —7 

f. _ interpret drawing in accordance with MIL-D- 7 D 327 _i. 

Z.~ IS.^/MACHINE FINISH ALL OVER - j 

3 .. MATERIAL: AL ALY £061 TEMP T£ ALT SPEC QQ-A -325 TEMP T£ WITHIN j 
1 - AREA INDICATED id 

^ Identify using drawing no., revision letter f manufacturers ..; 

LIT SYMBOL PER MIL-ST0-I3O - .1__T- - — - -1" 1 „J 


QTY. 

NOMENCLATURE 

PART OR 

SPECIFICATION 

MATERIAL 

FIND 

REQO. 

OR DESCRIPTION 

IDENTIFYING NO. 

OR NOTES 

NO. 





UNLESS OTHERWISE SPECIFIED 

INGTR 

MIT 1 

UMENTATION LAM 1 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

CONTKACT 

NAS 9-153 




DATE 

approved jd/LU+iL 

TiFBT 

1001579 


- 1.005 ± 0 ° 50 / 

CHECKED 

n// 






1001578 


DO NOT SCALE THIS DRAWING 

APfp^EO 

• • • •• ••• ••• •• 

••••••• • • • • 

1001577 


MATERIAL: 

uU< 


f 

• ••••• ••• • • 

NEXT ASSY 

USED ON 

SEE NOTE S . 7 

MITjJIL 

APPROVAL t 

DATE 


APPLICATION 


A 

&ZE 



LIST OF FARTS AND MATERIALS 


BLANK. 
END FITTING 


SCALE 
• 2 /. 


I 


UNIT WT. 


CODE IDENT. 


- WTf -“ 

INSTRUMENTATION 

LABORATORY 


Camhip 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 


NASA DRAWING NO. 


IOOI575 


SHEET / OF | 


I 


1 




INCHES 

. 1 . 


0 I 2 

PHOTOGRAPHIC SCALE ONLY 




* X 


I -! 


R'm-M 


r :lf 


*• 11 


;i , 



























! 


MOTES'. . ... - --—- f 

Interpret drawing in accordance with mil-d- 703E7 —i 

2. IDENTIFY USING DRAWING NO., REVISION LETTER (MANUFACTURERS 

‘ SYMBOL PER MtL-STD-130 ' - _ i 

3. MATERIAL- : AL AL.T 60G\ TEMP TG : __ ^ 

-—p . _... PER SPEC QQ-A-S2.5 TEMP T6 






UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

- 1.005 - 



1001579 


1001578 


DO NOT SCALE THIS DRAWING 

1001577 


MATERIAL: 

SEE: NOTE 3 

NEXT ASSY 

USED ON 


APPLICATION 



SHEET I 


Of l 

































i 


fjfc. <8 WW »»h 


- 'I*#4)?iJfli-»"•»,» ''i*', .!*•'!(*, - tfrtUtJkm-* 


1 


ZONE 


1 «"■ 1 




DESCRIPTION 


| DATE | APPROVAL 



NOTES'. ~L ■“ . ... — . : ““... ___ .• ■’ J 

t . INTERPRET DRAWING IN ACCORDACE WITH MIL-D-70327 ZZ — - 

£ OWELD:P(?OPIETO(?Y PROCESS OF SEANWEX CO.,INC.,LONG ISLAND CITY,NX,NY. 4 

а. ANODIC COAT PER MIL-A-8G25 TYPE I,CLEAR .— ...ZZZZZ Z. Z. ZZ....Z 

4-. PRESSURE TEST: ASSY MUST NOT DEFORM "WHEN PRESSURIZED TO 30 PSI6 i ; 

" "WITH DISTILLED WATER . . ’ Z ZZ ZZ" ZZ"": Z “Z 

5.ZLEAK TEST WITH HEUUM AT 77.5 t.S P31 A; MAXIMUM HEUUM LEAK. 110”° STD CC/SEC 
r CAFTER PRESSURE TEST) Z " Z... .!.Z Z- 4 

б. /cleaning (later) :zz:z:zzz::zz::zzzz zzzzz 

7 IDENTIFY USING DRAWING NO. REVISION LETTER / MANUFACTURERS PER MIL-5T0-13O 


1001581 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


QTY. 

REQO. 


BLANK,ENID FITTING 


HOSE,FLEXIBLE SEAMLESS 


COLLAR FLEXIBLE MOSE 


[TUBE, ALUMINUM 


NOMENCLATURE 
OR DESCRIPTION 


1001575 


\OOOZlS-Z 


I00157G 


1000250 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


FI NO 
NO. 


LIST OF PARTS AND MATERIALS 


MIT 

•MGYNUMCNTATION LAM 

OOHTRACT 



NAS 9-153 r DATE ' 

I * I I 




V 

ITVIL A PP R OVAL | DATE 


MIT/IL AP 

JW 




zz hose flexible: 

WELDING ASSY 

SPACECRAFT JT Q OPTICS BASEl 


SCALE 

i-t 


UNIT WT. 


CODE IDENT. 


HTT 

INSTRUMENTATION 

LA&OkaTORY 
_Camhipok. Maw._ 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001577 


SHEET 


OF \ 


'WMfcfesr. •■’A-*- 




I 



INCHES 1 

1 ■ 

• . i . i . i 

0 

1 2 

PHOTOGRAPHIC SCALE ONLY J 





















-WELD - 2. PLACES 
SEE MOTE Z 


o_ 

)8 


DNG ISLAND CITY, NY.,MY 

SURGED TO 90 P5»0 WITH DISTILLED WATER 

IELIUM LEAK -lO 8 STD CC/SEC (AFTER PRESSURE TEST} 


NOMENCLATURE 
OR DESCRIPTION 


LIST OF PARTS AND MATERIALS 



HOSE FLEXIBLE . 
WELDING ASSY 

OPTICS BASE TO I.M.U. 


CODE IOENT. 



1-1 


































































notes: .- —' - ------ - -- 

L INTERPRET DRAWING IN ACCORDANCE WITH MIL-0-7O327 : 

2. WELD*. PROPRIETARY PROCESS OP SEAMV.EX CO. INC. LONG ISLAND CITY, NY, NY 

3. ANODIC COAT PER MIL-A-0G25 TYPE I, CLEAR 

A. PRESSURE TEST .ASSY MUST NOT DEFORM WHEN PRESSURIZED TO SO PS»G 
WITH DISTILLED WATER 

5. LEAK TEST WITH HELIUM AT 77.5 t.S PSIA*, MAXIMUM HEUUNI LEAK - I O'® STD CC/SEC. 
; CAFTER PRESSURE TEST* 
fc. CLEANING*. 

Tl IDENTIFY USING DRAWING NO.,REVISION LETTER 4 MANUFACTURERS SYMBOL PER 
t MlL-STD-130_ _ . 

































NOTES*. . : . ... . ... ."2”. 

t INTERPRET DRAWING IN ACCORDANCE WITH MIL-0-70377 ~ 

fe IDENTIFY USING DRAWING NO.,REVISION LETTER MANUFACTURERS SYMBOL PER MIL-STD-ISO ~ 
S, COUPLING ^ QUICK DISCONNECT TO BE MACHINED T ASSEMBLED AS A PROPRIETORY PROCESS BY 
T SEATON WILSON MFG. CO. BURBANK,CALIF. ~ ri— 

4. THIS ASSEMBLY MUST MEET REQUIREMENTS OP PS IOOOI35. EXCEPT PRESSURE TEST. 

& PRESSURE TEST COMPLETE ASSEMBLY TO SO PSIG WITH DISTILLED WATER 

ft. LEAK TEST*. PRESSURIZE WITH HELIUM TO 77.5 1.5 P5IA *, MAXIMUM ALLOWABLE HELIUM LEAK 

: RATE SHALL BE 10‘ 8 STD C£J SEC. (AFTER PRESSURE TEST) 

7. COUPLING QUICK DISCONNECT MUST MATE WITH NASA PART NO. IOOOI35 
& MATERIAL*. MAKE FROM NASA PART NO 1001570 







































-pyifm 


2 


ZONE I SYM 


DESCRIPTION 


/ 


SEE NOTE 9 
REF 


rSEE MOTE 3^4 


•vTSt: 




notes: ' —....—---'.....— : ■■■' ..! 

C INTERPRET DRAWING IN ACCORDANCE WITH MIIL-D-70327 ’ 7 1 

E77IDENTIFY USING DRAWING NCX, REVISION LETTER <; MANUFACTURERS SYMBOL PER MIL-STD-130 
S. COUPLING, QUICK DISCONNECT TO BE MACHINED ? ASSEMBLED ASA PROPRIETORY PROCESS 

BY seaton wilson mfg.CO., burbank,cauF. ::777Z7777,77, 7,777777777777:777771., 7 

“THIS ASSEMBLY MUST MEET REQUIREMENTS OF PS IOOOI35 EXCEPT FOR PRESSURE TEST 
PRESSURE TEST COMPLETE ASSEMBLY TO SO PSIG WITH DISTILLED WATER 7~77IZ777 
7LEAK TEST! PRESSURISE WITH HELIUM TO 77.St.S PSIA.MAXIMUM ALLOWABLE . : 

^ HELIUM LEAK RATE SHALL BE lO' 8 STD CC/SEC (AFTER PRESSURE TEST) - 

XTtOUPLING,QUICK DISCONNECT MUST MATE WITH NASA PART NO. 1000135 7,17117:71777:: 

8. MATERIAL’. MAKE FROM NASA PART NO. 1001577 - 7:77 .7 777 7:777 77 

• 9. CONFIGURATION AND DIMENSIONS CONTROLLED BY ICO MH0I-0I008-II6 ..7' : : 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


foctFICATlON 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

D'MCNSIOm ARC IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


SEE NOTE 8 


MIT 

I NSTR UMENTATION LAB 
CONTRACT 


LIST OF PARTS AND MATERIALS 

: HOSE 

FLEXIBLE ASSY 

SPACECRAFT TO OPTICS BASE 

SCALE I UNIT WT. I CODE IDENT. 


INSTRUMENTATION 
LABORATORY 
Camhionk. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING Na 

IOOI581 


APPLICATION 


3 




































11.68 


notes: ...". .““ ............ 

L INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 T 

Z. IDENTIFY USING DRAWING NO., REVISION LETTER tf MANUFACTURERS SYMBOL PER MIL-STD-I30 
£, COUPLING, QUICK DISCONNECT TO BE MACHINED £ ASSEMBLED AS A PROPIETORY PROCESS BY! 

; SEATON WILSON MFG CO. BURBANK,CALIF. i 

K THIS ASSEMBLY MUST MEET REQUIREMENTS OF PS 1000155 EXCEPT PRESSURE TEST 

5 PRESSURE TEST COMPLETE ASSEMBLY TO SO PSVG WITH DISTILLED WATER. .j 

LEAK test: PRESSURIZE WITH HELIUM TO 77.5 — .5 P5IA. MAXIMUM ALLOWABLE HELIUM j 

IT LEAK. RATE SHALL BE IO' 8 STD CC/SECRAFTER PRESSURE TEST) | 

7. COUPUNG, QUICK DISCONNECT MUST MATE WITH NASA PART NO. IOOOISS 
B. MATERIAL: MAKE FROM NASA PART NO. IOOI579 
3 CONFIGURATION AND DIMENSIONS CONTROLLED BY ICO MHOI-01006-116 








































I 


NOTES*- 

I. INTERPRET DRAWING IN ACCORDANCE WITH 
STANDARDS PRESCRIBED BY MlL-D-70327. 


mmmm 


REVISIONS TDRA 0652S 



SYM 

ZONE 

DESCRIPTION 

DATE 

APPD. 


2.MATERIAL*. COPPER-BERYLLIUM ALLOY STRIP 
PER QQ-C-533 COND ‘/i H- 
PRECIPITATION HARDEN. 


3.UNLESS OTHERWISE SPECIFIED*. 

A.ALL EDGES TO BE FULL ROUNDED. 


63/ 

B.SURFACE ROUSHUESS MUST NOT EXCEED <7. 


4.IDENTIFY USING DRYING NUMBER, 
REVISION LETTER &ND HANUFACTUPEP'S 
SYMBOL PER NIL-STD-130. 


n 


.113 

.117 


± 


.OI8_ 

.023 


1.240 


1.260 


-.195 


J.6SO_ 


r 


.251 

.249 


I.G30 


DfcSH 

NO. 

DIM "A" 

AT LEAST 

LESS THAN 

1 

.0075 

.0085 

2 

.0085 

.0095 

3 

.0095 

.0105 

4 

.0105 

.0115 

5 

.OhS 

.0125 

<o 

.0125 

.0135 

7 

.0135 

.0145 

8 

.0145 

■■VSIEEHBH 

9 

.0155 

.0165 

10 

T 0I65 

.0175 

It 

.0175 

.0185 

12 

.0185 

.0195 



4. n 

-K 


-.032 DIA MAX 
2 PLACES 


_ DETAIL B 
.. ALTERNATE 
SLOT DESIGN 


















1000008 

OL /000201 

NEXT ASSY 

USED ON 

| APPLICATION | 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 


FRACTIONS DECIMALS ANGLES 

+ — +.005+ — 

-“.005- 


DO NOT SCALE THIS DRAWING 


MATERIAL 

SEE NOTE Z 


CONTRACT NAS9-49T 


AC SPARK PLUG DIVISION, GMC 
MILWAUKEE. WISCONSIN_ 


ACSP PN 




CHECKED 




APPROVAL D A.MtZ/FeGl* 
APPROVAL 4aJL 2//***£_ 


NASA APPROVAI 
MIT APPROVAL 



MIL I077C—P 




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HOUSTON. TEXAS 



CONTACT, 


LIMIT SWITCH 

CODE IDENT NO. 

f 

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NOTES: 

■1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. PIPA CALIBRATION ASSEMBLY, I TEM@SHALL BE MATCHED TO THE PIP PREALIGNED 
ASSEMBLY ITEm(T)PER ATP 1000013. 

3. MARK SERIAL NO. OF ITEM(T)AT DESIGNATED AREA OF ITEMf?) 

4. IDENTIFY USING DRAWING NUMBER AND REVISION LETTER PER ND1002019. 

5 )TEM 2 TO BE ASSEMBLED ON NASA ASSY NO. 1007153 OR 1007154 WITH 
13-17 IN-LB OF TORQUE AT INERTIAL SUB SYSTEM LEVEL. 

6. FOR SPARES PROCUREMENT THIS ASSEMBLY MUST MEET THE REQUIREMENTS 

OF PS -1001598. 


2 





1 














NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. PIPA CALIBRATION ASSEMBLY, I TEM©SHALL BE MATCHED TO THE PIP PREALIGNED 
ASSEMBLY ITEM©PER ATP 1000013. 

3. MARK SERIAL NO. OF ITEM©AT DESIGNATED AREA OF ITEM© 

4. IOENTIFY USING DRAWING NUMBER AND REVISION LETTER PER ND1002019. 

5. ITEM 2 TO BE ASSEMBLED ON NASA ASSY NO. 1007153 OR 1007154 WITH 
13-17 IN-LB OF TORQUE AT INERTIAL SUB SYSTEM LEVEL. 

6. FOR SPARES PROCUREMENT THIS ASSEMBLY MUST MEET" THE REQUIREMENTS 
OF PS -1001598.. 













!?L'0002C 

NEXT ASSY 

USED ON 

1 APPLICATION 

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ZONE I SYM 


REVISIONS TX>RK 0794, 


DESCRIPTION DATE I APPROVAL 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. PI PA CALIBRATION ASSEMBLY* I TEN0SHALL BE MATCHED TO THE PIP PREALIGNED 
ASSEMBLY ITEM0PER ATP 10OOOIJ. 

3. MARK SERIAL NO. OF ITEM0AT DESIGNATED AREA OF ITEM0 

4 . IDENTIFY USING DRAWING NUMBER AND REVISION LETTER PER ND1002019. 

5. ITEM 2 TO BE ASSEMBLED ON NASA ASSY NO. 1007153 OR 1007154 WITH 
13-17 IN-LB OF TORQUE AT INERTIAL SUB SYSTEM LEVEL. 


FIFA CALIBRATION ASSY 
PIP PREALIGNED ASSY 

NOMENCLATURE 
OR DESCRIPTION 


1007009 

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PART OR 
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SPECIFICATION 


MATERIAL 
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1000005 DL1000201 


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LIST OF PARTS AND MATERIALS 

PULSED INTEGRATING 
EMDULUM $ CALIBRATION 
MODULE - 

SCALE I UNIT WT. I CODE IOENT. 


MIT/ll APPROVAL 


INSTRUMENTATION 
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APOLLO GAN Specification I 

PS1001598 I 


PROCUREMENT SPECIFICATION 


PULSED INTEGRATING PENDULUM AND CALIBRATION MODULE 


The purpose of this document is to establish the requirements for the procurement 
of the Pulsed Integrating Pendulum and Calibration Module for use in the APOLLO 
Guidance and Navigation Equipment, 


0/ 


Sate 



APOLLO GAN Specification 
PS1001598 


PROCUREMENT SPECIFICATION 


PULSED INTEGRATING PENDULUM AND CALIBRATION MODULE 


1, SCOPE 

1.1 PURPOSE. This specification establishes the requirements for the spares procurement 
of the Pulsed Integrating Pendulum and Calibration Module, Drawing 1001598, hereafter called 
the assembly, ra <A , 

2. APPLICABLE DOCUMENTS 

2.1 EFFECTIVE ISSUES. The following documents of the issue in effect on the date of 
this specification form a part of this specification to the extent specified herein. 

SPECIFICATIONS 


APOLLO GAN 


ND1002210 


FTM1007009 


PS1007009 


ATP1000013 


DRAWINGS 


APOLLO GAN 


General Specification for Procurement of APOLLO 
Guidance n 1 ^ Navigation Assemblies and Subasse mbl ies 

Final Test Method for PIPA Calibration Assembly 

Procurement Specification for PIPA Calibration Assembly 

Assembly Test Procedure for 16 Pulsed Integrating Pendulum 


Pulsed Integrating Pendulum and Calibration Module 


i I s**4 








APOLLO GAN Specification 

P&001598 

Cl MB k fUU«M 
TDRR 


PROCUREMENT SPECIFICATION 
FOR 

PULSED INTEGRATING PENDULUM AND CALIBRATION MODULE 


Reoord of Revtaione 


Data 

Revision 

Letter 

TDRR 

No. 

Pages 

Approvals I 

Revlied 

MIT 

NASA 






• 
























































This opacification ooneieta of page I 
to ill and 1 to 3 inclusive. 


f 








APOLLO G6N Specification 
PS1001588 


PROCUREMENT SPECIFICATION 
FOR 

PULSED INTEGRATING PENDULI ' AND CALIBRATION MODULE 


The purpose of this document is to establish the requirements for the procurement 
of the Pulsed Integrating Pendulum and Calibration Module for use in the APOLLO 
Guidance and Navigation Equipment. 



itsA/MSC ' 






APPROVED BY 


-- y - 


title 

SATE 

T>i<L 

8- 


TITLE 


DATE 


APOLLO G&N Specification 
PS1001598 


PROCUREMENT SPECIFICATION 
FOR 

PULSED INTEGRATING PENDULUM AND CALIBRATION MODULE 


1. SCOPE 

1.1 PURPOSE. This specification establishes the requirements for the spares procurement 
of the Pulsed Integrating Pendulum and Calibration Module, Drawing 1001598, hereafter called 
the assembly. 

2. APPLICABLE DOCUMENTS 

2.1 EFFECTIVE ISSUES. The following documents of the issue in effect on the date of 
this specification form a part of this specification to the extent specified herein. 

SPECIFICATIONS 

APOLLO G4N 

ND1002210 General Specification for Procurement of APOLLO 

Guidance and Navigation Assemblies and Subassemblies 

FTM1007009 Final T st Method for PIPA Calibration Assembly 

PS1007009 Procurement Specification for PIPA Calibration Assembly 

ATP1000013 Assembly Test Procedure for 16 Pulsed Integrating Pendulum 

DRAWINGS 

APOLLO G&N 


1001598 


Pulsed Integrating Pendulum and Calibration Module 4 


APOLLO G&N Specification 
PS1001598 


3. REQUIREMENTS 

3.1 GENERAL SPECIFICATION. Unless otherwise specified herein, all of the requirements 
of Specification ND1002210 shall apply as requirements of this specification. 

3.2 DESCRIPTION. The assembly consists of a Pulsed Integrating Pendulum (PIP) and a 
Pulsed Integrating Pendulous Accelerometer (PIPA) Calibration Assembly which are matched 
together in accordance with ATP1000013. 

The PIPA Calibration Assembly provides a means of coupling the PSA constant current source 
and its related control circuitry to the torque ducosyn windings of a particular PIP. 

3.3 FUNCTIONAL REQUIREMENTS. The assembly shall meet the requirements of Speci¬ 
fications PS1007009 and ATP1000013. 

3.4 PERFORMANCE AND PRODUCT CHARACTERISTICS 

3.4.1 Service Life 


3.4.1.1 Operating Life . The assembly shall meet performance specifications for at least 
2000 hours of operation, excluding the supplier's test time of the completed unit. 

3.4.1.2 Shelf Life . The assembly shall have a shelf life of at least 3 years, without operation, 
at ambient room temperature after final acceptance at the supplier's facility. However, the 
PIP shall be maintained at its proper operating temperature. 

3.4.2 Reliability . Design objectives require maximum reliability of the assembly during its 
period of useful life. Every effort shall be made to design and produce units capable of meeting 
a maximum failure rate of 8.3 failures per million hours. 


APOLLO G&N Specification 
PS1001598 


4. QUALITY ASSURANCE PROVISIONS 

4.1 GENERAL SPECIFICATION. Unless otherwise specified herein, all of the quality 
assurance provisions of Specification ND1002210 shall form a part of this specification. 

4.2 NASA ACCEPTANCE INSPECTION. The NASA acceptance inspection shall be in accord¬ 
ance with Specifications FTM1007009 and ATP1000013. 

5. PREPARATION FOR DELIVERY 

5.1 GENERAL. Preparation for delivery shall be in accordance with Specification ND1002210. 

6. NOTES. None. 


Notice: When APOLLO G&N drawings, specifications, or other data are used for any purpose 
other than in connection with a definitely related NASA procurement operation, NASA thereby 
incurs no responsibility nor any obligation whatsoever; and the fact that NASA may have 
formulated, furnished, or in any way supplied the said drawings, specifications, or other 
data is not to be regarded by implication or otherwise as in any manner licensing the holder 
or any other person or corporation, or conveying any rights or permission to manufacture, 
use, or sell any patented invention that may in any way be related thereto. 


RJM:lv 


3 



SHEET 


- bb^lUUI 







3 





1001599 





























NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. PULSE TORQUE GYRO CALIBRATE ASSEMBLY, ITEM @ SHALL BE MATCHED TO THE 
GYRO PREALIGNED ASSEMBLY ITEM (T) PER ATP-1007021. 

3. MARK SERIAL NUMBER OF ITEM (T) AT DESIGNATED AREA ON ITEM @ . 

4. IDENTIFY USING DRAWING NUMBER AND REVISION LETTER PER ND 1002019. 

5. HEM 2 TO BE ASSEMBLED ON NASA ASSY NO. 1007153 OR 1007154 
WITH 13-17 IN-LB OF TORQUE AT INERTIAL SUB SYSTEM LEVEL. 

6. FOR SPARES PROCUREMENT THIS ASSEMBLY MUST MEET THE REQUIREMENTS 
OF PS-100) 599. 



REVISIONS 07*? 6 


ZONE SYM 


DESCRIPTION 


REVISED PER TDRR \3\&Z 
REVISED PER TDRR 13371 




- IPUL5E TORQUE GYRO CAL ASSY I 1007521-011 

1 PULSE TORQUE GYRO CAL ASSY 1007021 
1 Q-'PQ PtS^UOr-iED ASSV 1 I00CQI2 


iTEM Qty. 
NO. !"«#>• 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 



UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M I T 

INSTRUMENTATION LAB 
CONTRACT 


APPROVED FQR MSC 

A/tJ ?/ 


LIST OF PARTS AND MATERIALS 

OTO £ CALIBRATION 
MODULE ' 


MIT/IL APPROVAL 




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INSTRUMENTATION 
LABORATORY 
Camrridoc. Mam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 
































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APOLLO GCN Specification 
PS1001599 


PROCUREMENT SPECIFICATION 
FOR 

GYRO AND CALIBRATION MODULE 


The purpose of this document is to establish the requirements for the procurement of the 
Gyro and Calibration Module for use in the APOLLO Guidance and Navigation Equipment. 



S/MSC APPROVAL 



r'zrvrr v**' v 


3?'4* w* ; v iMw 

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APOLLO GAN Specification 
PS1001599 


PROCUREMENT SPECIFICATION 
FOR 

GYRO AND CALIBRATION MODULE 


1. SCOPE 


1.1 PURPOSE. - This specification establishes the requirements for the spares procurement 
of the Gyro and Calibration Module, Drawing 1001599, hereafter called the assembly. 


2. APPLICABLE DOCUMENTS 


2.1 EFFECTIVE ISSUES. The following document® of the issue in effect on the date 
of the specification form a part of this specification to the extent specified herein. 


SPE Cl FI CATIONS 
APOLLO GIN 


ND1002210 

General Specification for Procurement of 
APOLLO Guidance and Navigation Assemblies 


and Subassemblies 

ATP1007021 

Assembly Test Procedure for Pulse Torque 
Gyro Calibrate Assembly 

FTM1007021 

Final Test Method fo* Pu$fB Torque Gyro 
Calibrate Assembly ; 

PS1007021 

Procurement Specification for Pulse f'orque 
Gyro Calibrate Assembly 


PUBLICATIONS 

MIT/IL 

R-348 


Specification for Procurement of APOLLO Inertial 
Reference Integrating Gyro 





























APOLLO GAN Specification 

PSl001599 

Clans A Release 

TDRR I \i* & \ 


PROCUREMENT SPECIFICATION 
FOR 

GYRO AND CALIBRATION MODULE 


Reoord of Revisions 


Date 

Revision 

Letter 

TDRR 

No. 

Pages 

Revised 

Approvals \ 

MIT 

NASA 






























































This speoifloatton oonslsts of page i 
to ill and 1 to 4 Inclusive. 








APOLLO GAN Specification 
PS1001599 


PROCUREMENT SPECIFICATION 
FOR 

GYRO AND CALIBRATION MODULE 


The purpose of this document is to establish the requirements for the procurement of the 
Gyro and Calibration Module for use in the APOLLO Guidance and Navigation Equipment. 



APOLLO GIN Specification 

PS1001599 



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APPROVED BY 

TITLE 

DATE 

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APPROVED BY 


TITLE 


DATE 



APOLLO G4N Specification 
PS1001599 


PROCUREMENT SPECIFICATION 
FOR 

GYRO AND CALIBRATION MODULE 


1. SCOPE 

1 1 PURPOSE. - This specification establishes the requirements for the spares procurement 
of the Gyro and Calibration Module, Drawing 1001599, hereafter called the assembly. 

2. APPLICABLE DOCUMENTS 

2 1 EFFECTIVE ISSUES. The following documents of the issue in effect on the date 
of the specification form a part of this specification to the extent specified herein. 

SPECIFICATIONS 


APOLLO G&N 


ND1002210 

General Specification for Procurement of 

APOLLO Guidance and Navigation Assemblies 
and Subassemblies 

ATP1007021 

Assembly Test Procedure for Pulse Torque 

Gyro Calibrate Assembly 

FTM1007021 

Final Test Method for Pulse Torque Gyro 

Calibrate Assembly 

PS1007021 

Procurement Specification for Pulse Torque 

Gyro Calibrate Assembly 

PUBLICATIONS 


MIT/IL 


R-348 

Specification for Procurement of APOLLO Inertial 
Reference Integrating Gyro 


1 


APOLLO G&N Specification 
PS1001599 


DRAWINGS 

APOLLO G&N 


1001599 


Gyro and Calibration Module 


APOLLO G&N Specification 
PS1001599 


3. REQUIREMENTS 

3.1 GENERAL SPECIFICATION. Unless otherwise specified herein, all of the requirements 
of Specification ND1002210 shall apply as requirements of this specification. 

3.2 DESCRIPTION. The assembly consists of an Inertial Reference Integrating Gyro (IRIG) 
and a Pulse Torque Gyro Calibrate Assembly which are matched together in accordance 
with ATP1007021. 

The Pulse Torque Gyro Calibrate Assembly provides a means of coupling the PSA constant 
current source and its related control circuitry to the torque ducosyn windings of a particular 
gyro. 


3.3 FUNCTIONAL REQUIREMENTS. The assembly shall meet the requirements of Speci¬ 
fication PS1007021 and Publication MIT/IL R-348. 

3.4 PERFORMANCE AND PRODUCT CHARACTERISTICS 

3.4.1 Service Life 


3.4.1.1 Operating Life. The assembly shall hieet performance specifications for at least 
2000 hours of operation, excluding the supplier's test time of the completed unit. 

3.4.1.2 Shelf Life. The assembly shall have a shelf life of at least 3 years, without operation, 
at ambient room temperature after final acceptance at the supplier's facility. However, the 
gyro shall be maintained at its proper operating temperature. 

3.4.2 Reliability. Design objectives require maximum reliability of the assembly during 
its period of useful life. Every effort shall be made to design and produce units capable of 
meeting a maximum failure rate of 13.8 failures per million hours. 


3 


APOLLO GW Specification 
PS1001599 


4. QUALITY ASSURANCE PROVISIONS 

4.1 GENERAL SPECIFICATION. Unless otherwise specified herein, all of the quality 
assurance provisions of Specification ND1002210 shall form a part of this specification. 

4.2 NASA ACCEPTANCE INSPECTION. The NASA acceptance inspection shall be in 
accordance with Specification FTM1007021 and Publication M1T/IL R-348. 

5. PREPARATION FOR DELIVERY 

5.1 GENERAL. Preparation for delivery shall be in accordance with Specification 
ND1002210. 

6. NOTES. None. 


Notice: When APOLLO GfiN drawings, specifications, or other data are used for any 
purpose other than in connection with a definitely related NASA procurement operation, 

NASA thereby incurs no responsibility nor any obligation whatsoever; and the fact that 
NASA may have formulated, furnished, or in any way supplied the said drawings, specifications, 
or other data is not to be regarded by implication or otherwise as in any manner licensing 
the holder or any other person or corporation, or conveying any rights or permission to 
manufacture, use, or sell any patented invention that may in any way be related thereto. 


RJM/dmh 


4 


ZONE SYM 


REVISIONS 

DESCRIPTION 


DATE I APPROVAL 


A 1 REVISED PER TDRR \A-7-S> 


-TERM7r-TERM 9 
r-R 15 ■* 


SEE NOTE 4 
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j. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 
t. UNLESS OTHERWISE NOTED! 

I I ALL RESISTOR VALUES ARE IN OHMS 

| ALL CAPACITOR VALUES ARE IN t|FD > 

3. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN 
ACCORDANCE-WITH MIL-STD-440, 

WITH SN60WARP? SOLDER PER QQ-S-S7I 

4 . USE ATTACHED LEADS(LEAD IDENTIFICATION PER DWG N0.I00I60I). 

5. FOR INFORMATION REGARDING R3, R4, R5, R6, R7, R8,RI2 
: RIS, RI6, RI7 AND RI9 SEE NOTES ON. DRAWING 1001614- 


ADDITI ONAL 
CONNECTIONS 

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NOMENCLATURE 
OR DESCRIPTION 


_ 10106711-13 _ 

PART OR tKOFKiTMi 

I IDENTIFYING NO. 

LIST OF PARTS AND MATERIALS 


_ 1001614 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


MIT 

INSTRUMENTATION LAB 

CONTRACT 


WIRING ASSEMBLY 

CAL ARM AMPLIFIER") 


CODE IDENT. 


T/lt APPROVAL | DATE 

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notes: -.... ' . " ' . 

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UNLESS OTHERWISE NOTED! j. 
j ALL RESISTOR VALUES ARE IN OHMS 

! ALL CAPACITOR VALUES ARE IN UFD > 

3. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN 

. ACCORDANCE-.WITH MIL-STD-440, ' ‘ 

WITH SN60WARP2 SOLDER PER QQ.-S-57I 

4 . USE ATTACHED LEADS -- 7 

5. ^OR INFORMATION REGARDING R3, R4, R5, R6, R7, R8.RI2 
f RIS, RI6, RI7 AND RI9 SEE NOTES ON- DRAWING 1001614 


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4 


|A/R| WIRE 


NOMENCLATURE 
OR DESCRIPTION 


10106711-13 

PART OR 
IOENTIFYINQ NO. 


tPCCtfICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARC IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


1001614 


APPLICATION 


M IT 

IMCTftUMENTATtON LAS 
CONTRACT 


n I ac.<o. I 
nib Vo^MSC 

fylt APPROVAL | 

■VaZk- 2-Vi 


LIST OF PARTS AND MATERIALS 

WIRING ASSEMBLY 

(ALARM AMPLIFIER") 

■scale I UNIT m. I CODE IOENT. 


INSTRUMENTATION 
LABORATORY 
qi w wrm. WUam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA ORAWING NO. 

1001602 


3 










































4 



t / 






WINDING DATA 

TOTAU' NUMBER WINDINGS 7 _ 

WINDING ItiidmcI AWG TYPE OF I ENDING RESIS- 


LEADS 


WINDING -moKjc AWG TYPE OF ^inl^ -,- ^KiT.r.r at.^m 

NO. TURNS WjRE SIZE W|NDING TANCE(REF) length size . identification . 

_1° 0HMS-20aAT 2&C _START I FINIS! 


RANDOM 

RANDOM 

RANDOM 

COMMON 


£" 30 


FINIS H 

2 

4 


NOTES 

1. INSULATE BETWEEN WINDINGS NO I & NO 2 WITH A 005 POLYESTER 
WASHER ^ PER MIL-I-G3I TYPE G 

2. TURNS OR TURNS RATIO TOLERANCE tl% 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE 

4 . PREHEAT WINDING AND IMPREGNANT TO 250*F. IMPREGNATE 
WINDING WITH IMPREGNANT#,PULL NO VACUUM.BAKE 24HRS 
AT 180° F. 

5. (■) DENOTES THE SAME INSTANTANEOUS POLARITY 

6. WIPE IMPREGNATION DURING CURE CYCLE 

7. THE RESISTANCE BETWEEN -WINDINGS SHALL. NOT. BE LESS 

* , THAN 10 MEGOHMS WHEN MEASURED AT 250. VOLTS DC. 

AFTER BAKING 

8. BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A MINIMUM OF 
5 DAYS PER ND 1002209. CORE MUST MEET PERFORMANCE 
REQUIREMENTS OF SCD 1010689-2 AFTER TEMPERATURE CYCLING. 


SEE NOTE 5- 


SCHEMATIC 


^(jWDG^J 10 


7<XVDG408 


5<?VDG 30 6 


CORE I 


lowDG 102 3oWDG 204 


.CORE 2 



.51 DIA 
MAX 


H- 31 «N 

Tr-flifr r iT 

•I ••III II 





UNUM OJHCRWMC WECIHEO 


ZONE I SYM 


REVISIONS 

DESCRIPTION 


A/RI WIRE 
A7R IMPREGNANT 
A/R POLYESTER 
A7R WIRE (LEADS) 
A/R WIRE 
2 CORE 


1006711-18 
1010687-1 

1006711-13 

1006711-22 

1010689-2 


DATE I APPROVAL 


NOMENCLATURE 
OR DESCRIPTION 


i | identifying no. j tPgctFICATK)f< 

LIST OF PARTS AND MATERIALS 


NOTE 4iS 
NOTE I 
SEE DATA 
SEE DATA 


MATERIAL 
OR NOTES 


MIT 

INSTRUMENTATION LAS 


NEXT ASSY | USED ON 

APPLICATION 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

APTNOVED, 

contract 

mm 

DATE 

jj 2/ -4i 



CHECKED 

_ 


DO NOT SCALE THIS 

DRAWING 

— DRAWN 

! R.G S 

Vf MSC 

t M^'~ 

MATERIAL: 


~ HU 

2L, A; 




| iffr/IL APPROVAL | 

DATE 







CORE i COIL 
ASSEMBLY 

( REACTOR \ 

^SECOND STAGE) 


COOE tOENT. 


INSTRUMENTATION 

LABORATORY 

Caw«ip««. Ma—. 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO 

1001603 



















































ZONE I SYM 


REVISIONS 

DESCRIPTION 


WINDING DATA 


TOTAL NUMBER WINDINGS .6 

WINDING | TllDf l AWG V 
- NO. TURNS SIZE 


TURNS 

AWG WIRE 

TYPE OF 

WINDING 1 

RESISTANCE(RET) 


SIZE 

WINDING 

0HMS*20'/AT25C 

340 

41 

RANDOM 

17.8 

340 


RANDOM 

17.8 

500 


RANDOM COMM. 

43 

500 



46 

100 



10-3 

100 



10.5 


LEADS _ 

- I IDENTIFICATION 


NOTES 

1. TURNS OR TURNS RATIO TOLERANCE U%. 

2. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

3. PREHEAT WINDING i IMPREGNANT TO 250'F.,IMPREGNATE .WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24 HRS AT 180 F. 

4. (n) DENOTES THE SAME INSTANTANEOUS POLARITY 

5. WIPE IMPREGNATION DURING CURING CYCLE. 

6. BEFORE WINDING,TEMPERATURE CYCLE CORES FOR A Ml N I MUM OF 
5 DAYS PER ND-1002209. CORE MUST MEET PERFORMANCE 
REQUIREMENTS OF SCO 00688-2 AFTER TEMPERATURE CYCLING 

7 INSULATE BETWEEN WINDINGS NO. I £ N0.2 WITH A 005 POLYESTER 
WASHER .40 0SV.22 I.D. PER MtL-I-631 TYPE G 
: 8. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 
10 MEGOHMS WHEN MEASURED AT 250 VDC AFTER BAKING 



SEE NOTE 4- 


START 

I 

3 

5 

7 

9 

II 


FINISH 

2 

4 

6 

8 

10 

12 





.51 DIA 
MAX 



•31 U— 
MAX I | . 


A/R POLYESTER 

• 

NOTE 7 

A/R IMPREGNANT 

1010687-1 

NOTES 4(1 

A/R WIRE (LEADS') 

■1006711-13 

SEE DATA 

A/R WIRE 

1006711-22 

SEE DATA 

2 CORE 

1010688-2 


QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SB 


_ 1001614 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


00 NOT SCALE THIS DRAW! NO 
MATERIAL: 


_ LIST OF PARTS ANP MATERIALS 

CORE 6 COIL 
irlh ASSEMBLY 

\ £&\ (REACTOR FIRST STAGE) 

SCALE I UNIT WT. 1 CODE I DENT. 


tfflKWID 

CHECKED 

DAAWN 


It/il APPROVAL 


IHSTVtUM CNT ATION 
LABORATORY 
Cawwipw, Maw. 


MANNCO 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001604 




INCHES 


0 I 2 

PHOTOGRAPHKf SCALE ONLY 


nstsnassi 





























I ZONE I SYM 


REVISIONS 

DESCRIPTION 


WWWAL | I 


WINDING DATA 


TOTAL NUMBER WINDINGS 3 


WINDING 

NO 

TURNS 

TAP 

AT 

AWG WIRE ' 
, SIZE 

TYPE OF 
WINDING 

WINDING 

RESISTANCES 

0HMSt20%@25‘ 

PRI 

860 


41 

RANDOM 

54 

SECI 

200 

100 

36 

RANDOM 

3.9 

SEC 2 

340 

170 

41 

RANDOM 

' 25.8 


IDENTFICATION 


NOTES’- *> 

1 (■) DENOTES THE SAME INSTANTANEOUS POLARITY. _ ^ 

'2. PREHEAT WINDING AND IMREGNANT TO 250®fTTmPREGNATC WINDING. 

WITH IMPREGNANT. PULL NO \AOJUM.»BAKE 24 HRS AT 180° F. 

3, WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4 WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE tl^. ^ „ _ 1Ai . MrrrtLJMC 

6 THE RESISTANCE BETWEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS OC AFTER BAKING 
7. BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A MIMMlM OF 5 DAYS 
!* PER ND-10022 09. CORE MUST MEET PERFORMANCE 
I REQUIREMENTS OF SCD 1010689-2 AFTER TEMPERATURE CYCLING 


SCHEMATIC 


SEC I 
3 4 5 


SEC 2 
6 7 8 


SEE NOTE I 


— M,u uj 

i rr 


I 2 
PRI 


(_- 



.50 DIA 
MAX 


- _1 
> -J 


I 


Hi 

Hi 


A/R IMPREGNANT 
A/R WIRE (LEADS) 

A/R WIRE _ 

A/R WRE _ 

I CORE__ 


NOMENCLATURE 
OR DESCRIPTION 


00687-1 

1006711-13 

1006711-18 

1006711-22 

00689-2 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


NOTE 2 £4 
SEE CATA 
SEE DATA 
SEE DATA 


MATERIAL 
OR NOTES 


_ 1001614 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS OECIMALS ANQLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M IT 

INSTRUMENTATION LAS 
COMTfMCT 


list of parts and materials 

CORE & COIL 
ASSEMBIY 

(TRANSFORMER PWR) 

SCALE I UNIT WT. I COOE tOENT. 


Mn/IL APPROVAL 


•NSTRUM ENTATION 

LAMOftATORY 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXM 
NASA DRAWING NO. " 

DQ6C6 











































NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. SURFACE TO BE FLAT WITHIN 015 TIR . 

3. BRAZE PER MIL-B-7883 WITH CLASS4* SILVER SOLDER PER QQ-S-S6I 

4. FINISH-TIN PLATE PER MIL-T-10727 TYPE U (HOT DIP). 

5. RAN HEAD SCREW,CRES N0.4-40NC-2A X 5/16 LG PER MS 35233-14 













1001614 

NEXT ASSY 

USED ON 


APPLICATION 



PH OTOGRAPHKf SCALE ONLY 


















































ZONE I SYM 


DESCRIPTION 


113 *-003 
• -X)02 

2 HOLES 


DIA THRU 


.380 1 

.370 .875 
_ REF 


*1 -063 REF 



DIA THRU 


NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327 

2. BREAK ALL SHARP EDGES .010 MAX. 


lCASE. RECTANGULAR 


NOMENCLATURE 
OR DESCRIPTION 


1010691-2 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS OCCIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MIT 

INSTRUMENTATION LAS 
CONTRACT 


1001607 1100 1614 


APPLICATION 


LIST OF PARTS AND MATERIALS 


CASE MACHINED 


CODE IOENT. 


INSTRUMENTATION 
LABORATORY 
Cammipw. Mars. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001610 


INCHES 


PHOTOGRAPH)!? 3CALE ONLY 






























3 


| 

1 

1 

! 

j 

4 

t 

} 

I 

! 

i 





notes: ’ 

|. INTERPRET DRAWING IN ACCORDANCE WITH MILO-70327 
2. UNLESS OTHERWISE NOTED'. 


I! 



ALL RESISTOR VALUES ARE IN OHMS 
I ALL CAPACITOR VALUES ARE UFD 
3. SOLDERING OF ELECTRICAL CONNECTIONS 
j TO BE IN ACCORDANCE WITH MIL-STD-440, 
WITH SN60WARP2 SOLDER PER QQ.-S-57I 



9* 




s. 


i I 
! 


! 


I 

| 


i 


f 


4 


i 



\ 


3 


REVISIONS 


_ REVISIONS 

' _ DESCRIPTION 

REVISED PER TDRR Oi 



DIODE 

1010288-2 

IN058B 

DIODE 

1010286-1 

IN957B 

CAPACITOR 

1006755-135 

3.3 

RESISTOR 

1010694-222 

10 K 

RESISTOR 

1010694-97 

499 

RESISTOR 

1010694 —1 

49.9 

RESISTOR 

1010693-148 

1.69 K 

RESISTOR 

1010694-96 

487 

RESISTOR 

1010694-142 

\A7 K 

BOARD PRINTED CIRCUIT 

10016 1 3 



NOMENCLATURE 
OR DESCRIPTION 


I tDENTimN? NO. SPECIFICATION 

LIST OF PARTS AND MATERIALS 


_ 1001614 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FUNCTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M IT 

INSTRUMENTATION LAS 

CONTRACT 


CHECKED 

PRAWN 

APPROVED"* MSC 

WT/IL APP RO VAL I DATE 


PRINTED CIRCUIT 
BOARD ASSEMBLY 


CODE IDENT. 


1001611 

SHEET | OF \ 



MATERIAL 
OR NOTES 


MTT 

INSTRUM ENTATION 
LABORATORY 
CahmioMi Mars. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 


























I. INTERPRET DRAWING IN ACCORDANCE WITH MILH3-7CB27 
Z. UNLESS OTHERWISE NOTED'. 

| i ALL RESISTOR VALUES ARE IN OHMS 
| I ALL CAPACITOR VALUES ARE L|FD 

i Soldering of electrical-connections : 

| TO BE IN ACCORDANCE WITH MIL-STD-440, 
.WITH SN60WARP2 SOLDER PER QO-S-571 


REVISIONS 
























, .1 K$\ 

7 




«i-www* **mn*#***i-*m ''-.*»*** ^ * % *** 

4 I 3 


\ 1|c#«srL. " v* .V ■>- v* v ; fr" 


ACCEL Mil 6 

R 44 BRIDGE BRIDGE 

IK FEEDBACK CURRENT CURRENT 

NOTE S (COLLECTOR 2NI724) / "—v * 

-H8>—"0^>-tfiyi2>tfo)(My- 


t Rl 

X, IOK 


*L 8 > NOTE It 


I.47K 9 '4 7 | 


INPUT 9 REF (6 ) 
RESISTOR Y 


INPUT I REF (4 J 
RESISTOR Y 


I_ 


CRS NOTES 


(7) OUT PUT 
Y (BASE 2NI724) 


(9 ) COMMON (OV DC) 

Y (EMITTER 2NI724) 


• 7 • 


R6 

CR7 NOTE 10 


<D —cy- 

HI LO 

20VCT ±10% 

3200 CPS 
SO. WAVE 


NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-0*70327 

2. UNLESS OTHERWISE NOTEOJ 

ALL RESISTOR VALUES ARE IN OHMS 
ALL CAPACITOR VALUES ARE IN UFD 

3. REFER TO NASA DRAWING 1010039 

4. R3BR4 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 500 OHMS THRU 3K 

5. R5 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM IOK THRU SOK 
S.R7 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 2K THRU 20K 
7. R8 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 4K THRU 40K 
*RI2 TO BE SELECTED AT TEST 
RANGE OF VALUES FROM 200 OHMS THRU 5K 
% R15 TO BE SELECTED AT TEST 
RANGE OF VALUES FROM 50 OHMS THRU 300 OHMS 
KXR6 TO BE SELECTED AT TEST 
; RANGE OF VALUES FROM 50 OHMS THRU 100 OHMS 
II.RI9 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 500 OHMS THRU IOK 
I2.RI6S R17 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM 0 OHMS THRU 5K 


00 NOT t 

IQOIS 14 MMOMk 

USED ON 


REF 

DES 

PART NO. 

DESCRIPTION 

VALUE 

TOL 

RATING 

R 1 

1010694- 222 

RESISTOR 

IOK 

ll% 

I/IOW 

R2 

i - 222 


IOK 



R 3 

1010694 

NOTE 4 

SAT 



R 4 


4 




R5 


5 




R6 

1010693 

10 



1/4 W 

R7 

1010694 

6 



I/IOW 

R8 

1010694 

IF 7 

* 


j - 

R9 

1010693 “ 146 


I.69K 


1/4 W 

RIO 

1010694-96 


487 


I/IOW 

Rll 

1010694- 14 2 


I.47K 



R12 

1010694 

NOTE 8 

SAT 



RI3 

1010694 - 97 


499 



RI4 

1010694* 1 


49.9 



R 15 

1010694 

,, NOTE 9 

SAT 



CRI 

1010497 

DIODE 

500 PIV 


3.4W 

CR2 






CR 3 






CR4 






CR 5 






CRS 






CR 7 






CRS 



'l _ 



CR 9 

1010286-001 


6.8 V 

+ 5% 

400MW 

CRIO 

1010286*002 


7.5 V 

__±_ 

_L_ 

L 1 

1001604 

REACTOR 




L 2 

1001603 

4 




Tl 

1001605 

TRANSFORMER 




Cl 

1006755-135 

CAPACITOR 

3.3 

+ 10% 

IOV 

RI9 

1010694- 

RESISTOR NOTE II 

SAT 

11% 

I/IOW 

R16 


12 




R 17 


ir ,, 12 




RIB 

1010434- 3 

THERMISTOR 

1 K 

110% 



LIST Of PARTS AND MATERIALS 

SCHEMATIC 
'ALARM AMPLIFIER 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA MUSWNO NO. “ 

10016 12 




SHEET 






























™ ®(2)©@® 
®®(D©1 
WM ©®@®5 





B«J 

VIEW WITH COVER REMOVEO 


_ revisions OHXOfr 

ZONE STM DCSCWtmOW PATE | 

A RC.lf/'SE.D rOAA 05/26 



, ' l - 

I • 1.040 MAX _J 

■ -fV' 

'T* 


,203REFp5^ 


*©$<§>/ 


6 vs/ 4 V*/ 2^ 

9© 8 @) ©' 



-.203 REF 
TYP 


VIEW D*D 
ROTATED 90* 


VIEW C~C 
ROTATEO 90* 


INTERPRET DRAWING IN ACCORDANCE WITH MIL-0*70327 

R3 8 R4 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 

RANGE OF VALUES FROM 500 OHMS THRU 3K ^ ^ 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDEO. PER PART NO. 1010694 
IDENTIFY USING DRAWING NO., REVISION LETTER, SERIAL NO, AND 
MANUFACTURERS SYMBOL PER MIL-STD-130. 

ENCAPSULATE WITH EPOXY PER NO 1002036, CURING CYCLE • 

, ASSEMBLY TO MEET ALL REQUIREMENTS OF PS 1000283 

, SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE WITH MIL'STD-440, 
WITH SN60WARP2 SOLDER PER QQ" S’ 571 
, SOLDER COVER ASSEMBLY TO CASE PER MIL-S-6872A WITH 
SN50WARP2 SOLDER PER QQ-S*57I 

, MARK TERMINAL NUMBERS AS SHOWN PER NO 1002019 S NO 1002122 TYPE H CLASS I 
FINISH* VINYL- WASH PER MIL*C-I5328 AND ZINC CHROMATE PRIMER 
. FINISH, p.8585 a, PAINT BLACK SEMI-GLOSS ENAMEL TTE-529 CLASS B 

♦ COLOR 27038 PER FED STD 595 

I R5 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM IOK THRU 60K OHMS 

TWO RESISTORS MAY BE USEO TO GET VALUE NEEDEO. PER PART NO. 1010694 
. R8 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 

RANGE OF VALUES FROM 4K THRU 40K0HMS _. 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDEO. PER PART NO. 1010694 
RI2 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 200 OHMS THRU 5K OHMS . 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED* PER PART NO. 1010694 
J. R7 TO BE SELECTED PER ATPI00I6I4 AFTER INITIAL ENCAPSULATION 

?io 6 RE°S F .ST A 0 L R U S ES MA F Y R °B M E IsE^TO ISf °v!51e NEEDED. PER PART NO. 10.0694 
I. RI5 TO BE SELECTED PER ATP 1001614 PRIOR TO ENCAPSULATION 
RANGE OF VALUES FROM 50 OHMS THRU 300 OHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010694 
|. INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A *007 GRAY FIBER 
SHEET PER MIL-I-695A TYPE F WITH A MINIMUM DIELECTRIC STRENGTH 
OF 250 VOLTS PER MIL 

5. CENTER IDENTIFICATION PLATE OVER POTTING MOLE 
7. NUMBERS SHOWN FOR REFERENCE ONLY 

6. R6 TO BE SELECTED PER ATP 1001614 PRIOR TO ENCAPSULATION 
RANGE OF VALUES FROM 50 OHMS THRU 100 OHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDEO. PER PART NO. 1010693 


19. WINOING RESISTANCE FOR ACCEPTANCE TESTING: 

terminals; io a 11 isohms 130% 

12 a 13 5 OHMS 130% 

3 a 4 10.05KOHMS ±1% 

6 a 6 I0.05KOHMS il% 

20. RI6a RI7 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 0 OHMS THRU 5K0HMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010694 

21. RI9 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 500 OHMS THRU IOKOHMS. PER PART N0.I0I0694 


WIRING ASSEMBLY 

10016 0 2 


REF 

_ 

SCHEMATIC 

1001612 


REF 

— 

RESISTOR 

1010694 

SAT 

NOTE 20 

TT 


1010694 


NOTE 21 

20" 


1010694 


NOTE 20 

19 

RESISTOR, THERMAL 

1010434-3 

1 K 

iio% 

18 

GRAY FIBER SHEET 



NOTE 15 

TT 

RESISTOR 

1010694 

SAT 

NOTE 12 

7T 


1010694 


NOTE II 

15 


1010694 


NOTE 13 

14 


1010694 


NOTE 10 

13 


1010694 


NOTE 2 

12 


1010694 


NOTE 2 

II 


1010693 


NOTE 18 

10 


1010694 


NOTE 14 

9 


1007061 1010039 

NEXT ASSY WED ON 

APPLICATION_ 


1 00 NOT SCALE T 
MATKMAi: 


I MM ymn 

CHtcma I K— 

- —- I Lw*r 

» OWAWtNO tsntoviD ro* MSC 


DIODE 1010497 

TRANSFORMER 1001909 

REACTOR (SECOND STAGE) 1001603 

REACTOR (FIRST STAGE) 1001604 

PRINTED CIRCUIT BOARD ASS»Y~ 1001611 
CASE ASSEMBLY 1001607 

COVER ASSEMBLY 1001608 

PLATE- IDENTIFICATION 1001543 


_ LIST OF PARTS AND MATERIALS 

^TEMPERATURE ALARM 
2 a BACKUP CONTROL 
*4 AMPLIFIER ASSEMBLY 


UNIT WT. I coot WENT. 


fylL AffWOVAL | CATE 

LliM-U-tWA 


1001614 

T I » 1 

1 . 


PHOT UWAM i ftf *1 r ONLY 











NOTES 

(« INTERPRET DRAWING IN ACCORDANCE WITH NIL* 0-70327 
t* R3 0 R4 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 500 OHMS THRU 3K 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010694 
$• IDENTIFY USING DRAWING NO., REVISION LETTER, SERIAL NO, AND 
MANUFACTURERS SYMBOL PER MIL* STD-130. 

4, ENCAPSULATE WITH EPOXY PER ND1002036, CURIN6 CYCLE • 

9. ASSEMBLY TO MEET ALL REQUIREMENTS OF PS 1000283 

6. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE WITH MIL" STD* 440, 
WITH SN60WARP2 SOLDER PER QQ-S'571 

7, SOLDER COVER ASSEMBLY TO CASE PER MIL-S-6872A WITH 

SN50WARP2 SOLDER PERQQ-S*57I _ 

5. MARK TERMINAL NUMBERS AS SHOWN PER NO 1002019 & ND 1002122 TYPE H CLASS I 

9. FINISH*. VINYL- WASH PER MIL-C-15328 AND ZINC CHROMATE P«‘ME R 

PER MIL* P*8585A, PAINT BLACK SEMI-GLOSS ENAMEL TT-E‘529 CLASS • 
COLOR 27038 PER FED STD 595 

10. R5 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM IOK THRU 60K OHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010694 
It. R8 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 4K THRU 40K0HMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010694 
12 RI2 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 200 OHMS THRU 5K OHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED* PER PART NO. 1010694 

15. R7 TO BE SELECTED PER ATPI00I6I4 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 2K THRU 20K OHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010694 
14. RI5 TO BE SELECTED PER ATP 1001614 PRIOR TO ENCAPSULATION 
RANGE OF VALUES FROM 50 OHMS THRU 300 OHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010694 
IS INSULATE ELECTRICAL COMPONENTS FROM CASE WITH A .007 GRAY FIBER 
* SHEET PER Ml L ' 1 * 695A TYPE F WITH A MINIMUM DIELECTRIC STRENGTH 
OF 250 VOLTS PER MIL 

16. CENTER IDENTIFICATION PLATE OVER POTTING HOLE 

17. NUMBERS SHOWN FOR REFERENCE ONLY 

16. R6 TO BE SELECTED PER ATP 1001614 PRIOR TO ENCAPSULATION 
RANGE OF VALUES FROM 50 OHMS THRU 100 OHMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010693 


19. WINDING RESISTANCE FOR ACCEPTANCE TESTING: 

terminals; io a 11 1 3 ohms iso% 

12 a 13 5 OHMS ±30% 

3 a 4 10. 05KOHMS ±1%. 

S a 6 I0.05K0HMS ±1% 

20. Rt6 6Rl7 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 0 OHMS THRU 5K0HMS 

TWO RESISTORS MAY BE USED TO GET VALUE NEEDED. PER PART NO. 1010694 

21. RI9 TO BE SELECTED PER ATP 1001614 AFTER INITIAL ENCAPSULATION 
RANGE OF VALUES FROM 500 OHMS THRU I0K0HMS. PER PART N0.I0IO694 






1010694 


1010694 


1010434-3 


1— 




WMMIFl 


■?r*uikfcaii 



PLATE* IDENTIFICATION 


UMUH oTMcmmc manta 


__JliLii* 

I T2/JR I 

" III I ■ i I 


UST of parts ano materials 


TEMPERATURE ALARM 
a BACKUP CONTROL 
AMPLIFIER ASSEMBLY 


E3 


1)007081 110 10039 





APPLICATION 




































































REVISIONS ' _ 

ZONE SYM DESCRIPTION 0*TC APPROVAL 

a” REVISED PER TDRR 05125 n-lQ-i3 u)£ 


JO ft-ACES 




-IU 


040 MAX 


.5 MIN- 


notes: 

I. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED PER MIL-D-70327. 
2.SOLDERING PER MIL-S-6872A WITH SN50 WARP2 SOLDER PER QQ-S-571. 


A/R SOLDER _ 

10 TERMINAL _ 

I COVER-MACHINED 


NOMENCLATURE 
OR DESCRIPTION 


1010690 - > 
1001617 

PART OR 
lOENTlFYINQ NO. 


SPECIFICATION 


ISEENOTE 21 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M I T 

IN STR UMENTATION LAS 

CONTRACT 


LIST OF PARTS AND MATERIALS 


COVER ASSEMBLY 


11000286 


UNIT WT. 


CODE IDENT. 


T/IL APPROVAL 


INSTRUMENTATION 
LABORATORY 
Cam«hp—. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001616 


APPLICATION 


i 

































*& 4 |.-! 


4 



3 



2 


WPLACES 



I 




REVISIONS 


ZONE 


T^T 


DESCRIPTION 


€>*&< ,_ 

| 0*TI | APPROVAL 


S-! 

: 5fc 


; St* 

lit 


t 

; ■] 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. USE SOLDER SN50 PER Q.Q-5-571 



P f 

; t 













































































ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 

-- 

A 

H£W3£D 04-533 

tf-6-63 

MC. 




NOTES! 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

3. ENGRAVE OR METAL STAMP PER NO 100219 (.06 CHARACTERS). 

4 . FINISH-TIN PLATE PER MIL-T-10727 TYPE H (HOT DIP). 

; 5. BREAK ALL SHARP EDGES .010 MAX 



APPLICATION 


SHEET 


OF 






































































mtm 


REVISIONS 

DESCRIPTION 


S) ZONE SYM _ DESCRIPTION _ DATE 

^_ A /?£I//3£D P&K ro, /?/f 04533 0-6-63 ' 

^ B REVISED PER TDRR 05127 12-lO-tt' 


DATE I APPROVAL 


.830 REF- 


• l 33 -x>ol DIA THRU 10 H0LES 


^ |0 .030 DIA | 

SEE NOTES 2 8 3 


BSC 4 PLACES 


in 


:.I56 REF 


.019 REF 


.22 - .406 , 
'.20 ^BSC.' 


2 PLACES 


NOTES! 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

3. ENGRAVE OR METAL STAMP PER NO 10020198 ND1002122, TYPE D, CLASS 1, .06 CHARACTERS 

4. FINISH-TIN PLATE PER MIL-T-10727 TYPE H (HOT DIP). 

-5. BREAK ALL SHARP EDGES .010 MAX 


i 


COVER > RECTANGULAR 1010691 - 4 

NOMENCLATURE PART OR •pcnnTAnnii 

_ OR DESCRIPTION _ IDENTIFYING NO. M’ECltTCATiqw 

LIST OF PARTS AND MATERIALS 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 


M IT 

INSTRUMENTATION LAB 


1001616 1000286 
NEXT ASSY USED ON 

APPLICATION 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

CONTRACT 

CHECKED J5 ^ 

1 "datT 
g.2£ 

DO NOT SCALE THIS DRAWING 

— DRAWN A? S. V. 

__ APPROVED FOR MSC 


MATERIAL: 

//j fl&LZi/L 



& X 

Mn/N. APPROVAL 

(date 


COVER-MACHINED 


COOL I DENT. 


INSTRUMENTATION 

LABORATORY 

Ca mh ibm, Maw. 

owa. no. _ 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001617 

SHEET | OF | 













































ZONE I SYM 


DESCRIPTION 


DATE 


APPROVAL 



NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

3. ENGRAVE OR METAL STAMP PER ND 100219 (.06 CHARACTERS). 

4. FINISH-TIN PLATE PER MIL-T-10727 TYPE II (HOT DIP). 

,5. BREAK ALL SHARP EDGES .010 MAX 






UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS OECIMAIJS ANGLES 








DO NOT SCALE THIS DRAWING 


1000286 

MATERIAL: 

NEXT ASSY 

USED ON 


\ 

COVER,RECTANGULAR 

1010691-4 



> 

g 

QTY. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FINO 

NO. 

1 


LIST OF PARTS AND MATERIALS 
■ ---—-- 1 .. MIT 

■ 


M I T 

INSTRUMENTATION LAB 
CONTRACT 

NAS feate 

APPROVED 


CHECKED 


DRAWN 


/€’ V. -J 


iO • 2 'La 

tM 


9-3-6A 


APPROVED FOR MSC 


f/jQMLu/0-2-t3 

Mlf/IL APPROVAL DATE 


COVER-MACHINED 


SCALE 

2/1 


UNIT WT. 


COOE IDENT. 


INSTRUMENTATION 

LABORATORY 


MANNED 

SPACECRAFT CENTER 
MOUfTON TEXAS 


NASA DRAWING NO. 


IOOI6I7 


APPLICATION 


SHEET 






































































- WTf - 

IN8TKUM ENT ATION 
LABORATORY 

Cammidml Maml 

- 

OHM. NO. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DftAWINQ NO. 


1001618 


SHEET | OF | 

1 



“>!• 

iVtl 

it 

.fef ! 


■ *'*t 


" INCHES . 1 

| i | > 1 i 1 »- J v 

0 I >* ’8 'I 

PH0T0GRAPHK?8CAL£ ONLY 




















B 


if:.-'. er '"o i 


± 


Ml 

I 



| REVISIONS 1 

ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 


A 

REVISED PER TDRR 05128 

n-ii-ti 

~u/t~ 


B 

REVISED PER TDRR 06064 




notes: 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS. 

ALL CAPACITOR VALUES ARE IN UF. 

3. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN 
ACCORDANCE WITH MIL-S-6872 WITH SN60WRAP2 . 

SOLDER PER QQ-S-571. 




! • • • ! • • • 

;••• • • i * • 



UNLESS OTHERWISE SPECIFIED 

INSTR 

MIT 1 

UMENTATION LAN 1 



DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

CONTRACT 

NAS 




DATE 

APPROVED 






CHECKED 



drawn 



••••* I • •• 

• ••• • • 



DO NOT SCALE THIS DRAWING 

APPROVED 

FOR MSC 




1000286 

MATERIAL: 


2^T 


NEXT ASSY 

USED ON 


KflV/IL APPROVAL 

DATE 


APPLICATION 



2E 




QTY. 

REQO. 


DIODE 


CAPACITOR 


RESISTOR 


RESISTOR 


BOARD,PRINTED CIRCUIT 


NOMENCLATURE 
OR DESCRIPTION 


1010497 


1006755-19 


1010694-97 


1010695-126 


1001624 


PART OR 
IDENTIFYING NO. 


500 PIV 


3.3 


499 


IK 


SPECIFICATION 


3.4W 


15V 


I/IOW 


I/8W 


MATERIAL 
OR NOTES 


FIND 

NO. 


LIST OF PARTS AND MATERIALS 


PRINTED CIRCUIT 
BOARD ASSEMBLY 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


MTT 

IN«TNUI*»MTATION 
LABORATORY 
Camwidw. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA ORAWINQ NO. 

1001618 


SHEET | 


OF | 


1 




INCHES 
■1 till 


O I 2 

PHOTOGRAPHIC SCALE ONLY 



























notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. UNLESS OTHERWISE INDICATED', 

ALL RESISTOR VALUES ARE IN OHMS. 

ALL CAPACITOR VALUES ARE IN UF. 

3. USE SOLDER SN60 PER O r . "71. FOR ALL ELECTRICAL 
CONNECTIONS. 


2 




tm? 



REVISIONS 

firm—l 

ZONE | SYM | 

DESCRIPTION 

| DATE | APPROVAL 1 


i 

Ml 

f 


J 


D 


REF 

DES 

PART NO. 

DESCRIPTION 

VALUE 

TOL 

RATING 

KB 

1010364-252 

RESISTOR 

IK 

1% 

I/8W 

IQI 

-j - 



* _ 



|_i_ 

■nai 

1010311-97 



499 



I/IOW 

R6 

-1—“ 







_ 

R7 

1010311-164 



2.49K 

n 




Cl 

1006755-19 

CAPACITOR 

3.3 


15V_ 

C2 











C3 






_ 


r 


f 1 

CRI 

1010497 

DIODE 

UTR52 


3.4 W 1 

CR2 










CR3 






■ 




CR4 










CR5 

1010439 



HZ8883 


250 MW 

CR6 

1010497 



UTR52 


3.4 W 


.1._-_L_.~ X - 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


1000286 


NEXT ASSY 


USED ON 


APPLICATION 


MATERIAL: 


1 

BOARD,PRINTED CIRCUIT 

1001624 



QTY. 

NOMENCLATURE 

PART ON 

SPECIFICATION 

MATERIAL 

REQO. 

OR DESCRIPTION 

IDENTIFYING NO. 

ON NOTES 


LIST OF PARTS AND MATERIALS 


MIT 

INSTRUMENTATION 

CONTRACT 

NA S Wjaj 

LAN 

“daTT 

APPROVED ELrLstr\ 

/o 

CHECKED 



DRAWN 



APPROVED FOR MSC 

itfr/IL APPROVAL 

DATE 

VO 



T3T7T 


PRINTED CIRCUIT 
BOARD ASSEMBLY 


SCALE 


UNIT WT. 


CODE IDENT. 


NONE 


INSTRUMENTATION 

LABORATORY 

Camhiow, Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


1001618 

SHEET OF 


1 


' r.\.- ■ '-*4 


T 


i- 

i 

!. 


h 



Lz 







































































































ZONE SYM DESCRIPTION _ DftTC APPROVAL 

A REVISED PER TDRR 05129 U)tt 


Tl-I SEE NOTE 3 
TI-2 I ' 


ADDITIONAL 
CONNECTIONS 
NOTE 31 TCEM-f 


TI-2 TEKM-2 

RED I (Ll-I) TI-3 
RED 3 (LI-3) TI-5 

RED 6 (LI-6) TS2M-9 

RED 7 (LI-7) TEe/U-3 
RED 8 (L2-8) T£e*t-4 

RED 9 (LI-9) TEeAT-6 
RED 10 ~ (L2-I0) TEEMS 
GRN6 "(L2-6) R7 


TERMINALS’ 


TERMINAL 7 


TERMINAL 10 - 


-► GRN 4 
SEE NOTE 3 


'.nJ VF 


or ss 


R4 SEE NOTE 5 


j±5'p;/o o 6 ) 


—► GR2 
SEE NOTE 3 


/ TI-4 
I SEE NOTE 3 

4 JUMPER 


' L^R3-^ \ 

SEE NOTE 5 ' 


RED i 

SEE NOTE 3 


RED 4 

SEE NOTE 3 


NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE WITH MIL-STD-440, 
WITH SN60 WARP2 SOLDER PER QQ-S-571. 

3. USE ATTACHED LEADS. 

4. UNLESS OTHERWISE INDICATED; 

™ ALL RESISTANCE VALUES ARE IN OHMS. 

ALL CAPACITANCE VALUES ARE IN UF. 

JL FOR HJFORMAT/Otf REGARD/NG R? , 24 AND E? -SEE ——~ 

_ - . Notes o/Jdraia/iAg /oooe&g 


Ia/rI wire 


I'lO 0671H3 AWG 30 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 

IDENTIFYINQ NO. ! 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 


MIT 

INSTRUMENTATION LAS 


_ 1000286 

NEXT ASSY USED ON 

APPLICATION 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 


CONTRACT 

N> s « 53 

DATE 

FRACTIONS DECIMALS ANGLES 

APPROVED 

CHECKED 

— DRAWN 

/Sc,ru£& 

e. </• 


DO NOT SCALE THIS DRAWING 

APPROVED 

TOR MSC 


MATERIAL: 

~ m { 

A 

r.K J 



APPROVAL 

| DATE 


LIST OF PARTS AND MATERIALS 

WIRING 

ASSEMBLY 

ale I UNIT WT. I CODE IOENT. 


INSTVtUM €NTATK>N 
LABOF.ATORY 
Cammipw, Ma—. 

PUR. WO, 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA ORAWING NO. 






















3 


2 


ZONE STM 


REVISIONS 

DESCRIPTION 


_£3_£6£_ 

| DATE 



ADDITIONAL 

CONNECTIONS 

Tl-l SEE NOTE 3| TLEM-t 

TI-2 

11 T££M~2 

RED 1 

TI-3 

RED 3 

TI-5 

RED 6 

T££A4-9 

RED 7 

T£2M~5 

RED 8 

TSEM-6 

RED 9 

TEEM-7 

RED 10 

H TEEMS 


TERMINAL-4* 


TERMINAL 3 


GRN 6-*—\ 
SEE NOTE 3 


• CR4 (+) 


GRN 4 

SEE NOTE 3 


TERMINAL 10* 


(w 


1 1 
» 'S' VI 


R4 SEE NOTE 5 


J 4 jp;/o 6 6) 


—►GR2 
SEE NOTE 3 


/ TI-4 
rSEE NOTE 3 

4 JUMPER 


'^►R3-^\ 

SEE NOTE 5' 


RED 2 

SEE NOTE 3 


RED 4 

SEE NOTE 3 


NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. ALL ELECTRICAL CONNECTIONS TO BE MADE WITH SN60 SOLDER 
PER QQ-S-571. 

3. USE ATTACHED LEADS. 

4. UNLESS OTHERWISE INDICATED; 

ALL RESISTANCE VALUES ARE IN OHMS. 

ALL CAPACITANCE VALUES ARE IN UF. 

- y. FOR rt/FORMAT/oN -REGARDING, R3 j R+ SEE . 

Notes Ofi draining iooossg 


NOMENCLATURE 
OR DESCRIPTION 


10106711-13 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


_ 1000286 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL 


M IT 

INSTRUMENTATION LAS 
CONTRACT 

_ mas jWfr ["DATE 

CHECKED f'Jorj 

PR AWN l/P. vw, 1-n-L 

APPROVED FOR MSC 


LIST Of PARTS AND MATERIALS 

WIRING 

ASSEMBLY 


INSTRUMENTATION 
LABORATORY 
Camwipee. Maw. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 


UNIT WT. 


COOE IDENT. 


IOOI619 


3 


2 


1 

























































MJl ZONE I SYM 


DESCRIPTION 


DATE I APPROVAL 


A I /?£!//$£/> PEA 7TD/VT Q5/3Q 


_ INTERCONNECTIONS 

LI-KSEE NOTE2)1 L2-I ~ 
LI-3(SEE NOTE 2) L2-3 
LI-5(SEE NOTE 2) L2-5 


RED (LI) 


GREEN (L2)- 



SEE NOTE 


6.00 MIN 
4 LEADS 


-SEE NOTE 10 


LEAD IDENTIFICATION 
ON SCHEMATIC I ON REACTOR 

Ll-I _ RED I 

LI-2 _ RED 2 _ 

LI-3 _ RED 3 _ 

LI-4 _ RED 4 

LI-6 _ RED 6 _ 

L2-2 _ GREEN 2 

L2-4 GREEN 4 

L2-6 [GREEN 6 

[WINDING RESISTANCE (REF) I 


SEE NOTE 9QYT 


.50 DIA 
MAX 


-SEE NOTE 7 

START OF WINDING 


SEE NOTE 10- 


3 PLACES 


5 PLACES 


6.00MINh—.88 MAX- 


-6.00 MIN- 


t 20% 


NOTES: 

1. 

2 . 

3. 


25° C _ 

I OHMS 
39 
39 

39 ~ 

39 ~ 

400 

0.02 MAX 
0.02 MAX 


INSULATE BETWEEN REACTORS WITH 002 MYLAR TAPE PER MIL-1-15126. 

BRING OUT ONE LEADWIRE. 

PREHEAT WINDING AND IMPREGNANT TO 250“F. IMPREGNATE WINDING WITH IMPREGNANT. 
PULL NO VACUUM. BAKE 24 HRS AT 180* F 
WIPE IMPREGNATION DURING CURE CYCLE. 

SET LEADS EQUALLY SPACED AROUND PERIPHERY. OF WIND|NG,WITH MYLAR 
TAPE PER MIL-I-15126,ORDER OPTIONAL. , 

-PART NO. 1001621 MUST BE A MATCHED PAIR. ' 

ADD TWO COMMON WINDINGS.ONE(I) TURN EACH. USE WIRE f^N 10106711-46. 

LEAVE 6 INCH WINDING WIRE FOR LEAD. IDENTIFY AS SHOWN. 

THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING 
ASSEMBLE REACTORS BACK TO BACK 

.WINDING'.LEAD “SET END" - • 

INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327 y 


A/R WIRE _ 

A/R WIRE (LEADS) 

A/R IMPREGNANT _ 

A/R TAPE _ 

2 CORE f COIL ASSY 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


1006711-46 

1006711-13 

1010687-1 

1001621 

PART OR 
IDENTIFYING NO. 


AWG 20 
AW G 30 


SPECIFICATION 


SEE N0TE7 
SEE NOTE 5 
SEEN0T E^4 
SEE NOTE I 
' Sg NOTE 6 

MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


1000286 


M • T 

INSTRUMENTATION LAS 

CONTRACT 

jwsy9>r53 ranr 


ilT/IL APPROVAL 


LIST OF PARTS AND MATERIALS 


REACTOR ASSEMBLY 


CODE IDENT. 


INSTKUM ENTATION 
LABORATORY 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING MX 

1001620 


APPLICATION 
































_I-- -— 1 -—- 

' & 

ZONE 

SYM 

REVISIONS O 3 <= 

DESCRIPTION 

r 

DATE 

APPROVAL 



A 

PEVIbPD PI'.P POPP 05/30 

p-tt-ii 




B 

REVISED PERTDRR 10799 

ie> jul 
64 

j 



| INTERCONNECTIONS I 

LI-LSEE NOTE2) 

L2-I 

LI-3(SEE NOTE 2) 

L2-3 

LI-5GEE r-TTE 2) 

L2-5 


LEAD IDENTIFICATION 

ON SCHEMATIC 

ON REACTOR 

LI -1 

RED 1 

LI-2 

RED 2 

LI-3 

RED 3 

LI-4 

RED 4 

LI-6 

RED 6 

L2-2 

GREEN 2 

L2-4 

GREEN 4 

L2-6 

GREEN 6 . 


WINDING RESISTANCE (REF) 
t 20% @ 25°C 

FROM 

TO 

OHMS 

LI" 1 

LI-2 

39 

LI- 3 

L 1- 4 

39 

LI- 1 

TF5 1 

3$ .. 

LI-3 

L2-4 

39 

LI-6 

L2-6 

400 

7 

8 

0.02 MAX 

9 

10 

0.02 MAX 


B 


notes: 

1. INSULATE BETWEEN REACTORS WITH .002 MYLAR TAPE PER MIL-1-15126. 

2. BRING OUT ONE LEADWIRE. mDD rrkiAkiT 

3. rrehEaT WINDING AND IMPREGNANT TO 250°F. IMPREGNATE WINDING WITH IMPREGNANT. 

PULL NO VACUUM. BAKE 24 HRS AT 180* F 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. SET LEADS EQUALLY SPACED AROJND PERIPHERY OF WIND|NG,VVITH MYLAR 
TAPE PER MIL-1-15126, ORDER OPTIONAL. 

6. PART NO. 1001621 MUST 5E A MATCHED PAIR. 

7. ADD TWO COMMON WINDINGS. ONE (I) TURN EACH. USE WIRE P/N 10106711-12,TWO STRANDS FOR EACH TURN. 
LEAVE 6 INCH WINDING WIRE FOR LEAD. IDENTIFY AS SHOWN. 

8. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING 

9. ASSEMBLE REACTORS BACK TO BACK 

10. WINDING LEAD “SET END" 

11. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MlL-D-70327 


A 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


1000286 


NEXT ASSY 


USED ON 


APPLICATION 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


T 


B 


A/R 

WIRE 

1006711-12 

AWG 23 

SEE N0TE7 

5 

A/R 

WIRE (LEADS) 

1006711-13 

AW G 30 

SEE NOTE 5 

4 

A/R 

IMPREGNANT 

1010687- 1 


SEE NOTE'JfA 

i 

A/R 

TAPE 



SEE NOTE 1 

2 

2 

CORE t r 0H ASSY 

1001621 


SEE NOTE 6 

1 

QTY. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 


LIST OF PARTS AND MATERIALS 


M 1 T 

INSTRUMENTATION 

CONTRACT 

LAB 

DATE 

approved/^ 1 

'•■2-LI 

CHECKED 


* 

DRAWN 

ze, / v. 

9-3-63 

APPROVED^TO*^ MSC 

ilT/lf. APPROVAL 

DATE 

A - it 



REACTOR ASSEMBLY 

- mTT - 

INSTRUMENTATION 

LABORATORY 

Camrridoc. Mam. 

OWQ. NO. 

MANNEO 

SPACECRAFT CENTER 

HOUSTON TEXAS 

NASA DRAWftfQ NO. 

1001620 

SCALE 

UNIT WT. 

CODE IDENT. 



SHEET 1 OF | ^ 


i i 


4 


3 


2 


1001620 |B| f 









RE-VIbEO PCX TOtt 05/30 

REVISED PERTDRR 10799 
REVISED PERTDRR 11668 


DATE APPROVAL 

16 JOL 

64 


INTERCONNECTIONS 
LI-KSEE NOTE 2)1 L2-I 
LI-3CSEE NOTE 2) L2-3 
LI-5 L2-5 


RED (LI) 
GREEN (L2)— s 



SEE NOTES 149 

r*—6.00 MIN —I 
4 LEADS 


•SEE NOTE 10 


LEAD IDENTIFICATION 
ON SCHEMATIC I ON REACTOR 

LI -1 _ RED I _ 

LI-2 _ RED 2 _ 

LI-3 _ RED 3 

LI-4 _ RED 4 _ 

LI-6 _ RED 6 _ 

L2-2 _ GREEN 2 

L2-4 _ GREEN 4 

L2-6 [GREEN 6 

WINDING RESISTANCE (REF) 
t 20% <S 25° C_. 


.50 DIA 
MAX 


SEE NOTE 10- 


3 PLACES 


6.00MIN 


SEE NOTE 7 

START OF WINDING 


5 PLACES 


88 MAX- 


-6.00 MIN- 


FROM 

TO 

OHMS 

LI* 1 

LI-2 

39 

LI* 3 

L 1- 4 

39 

LI- 1 

L2-2 

39 

LI-3 

L2-4 

39 

LI-6 

L2- 6 

400 


NOTES: 

I. 

i 2 . 

3. 


0.02 MAX 
0.02 MAX 


INSULATE BETWEEN REACTORS WITH .002 MYLAR TAPE PER MILT-15126. 

PRENE/^wmOING AN^MPREGKIANT TO 250°F. IMPREGNATE WINDING WITH IMPREGNANT. 

PULL NO VACUUM. BAKE 24 HRS AT 180” F 
WIPE IMPREGNATION DURING CURE CYCLE. - 

SET LEADS EQUALLY SPACED AROUND PERIPHERY OF WIND|NG,WITH MYLAR 
TAPE PER MIL-I-I5I26,ORDER OPTIONAL. 

PART NO. 1001621 MUST BE A MATCHED PAIR. 

ADD TWO COMMON WINDINGS. ONE(I) TURN EACH. USE WIRE P/N I0I067IM2, TWO STRAMDS FOR EACH TURN. 
LEAVE 6 INCH WINDING WIRE FOR LEAD. IDENTIFY AS SHOWN. 

THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING 
, ASSEMBLE REACTORS BACK TO BACK 

.WINDING'LEAD "SET END" 

, INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
’PRESCRIBED BY M I L* D *70327 


UNLESS OTHERWISE SPECIFIED 



A/R WIRE _ 

A/R WIRE (LEADS) 

A/R IMPREGNANT _ 

A/R JAPE_ 

2 CORE t COIL ASSY 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


1006711- 12 
1006711-13 
1010687-1 

1001621 ~~ 

PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAS 


1000286 
NEXT ASSY USED ON 

APPLICATION 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

APPROVED^ 

CONTRACT 

m 

DATE 



CHECKED 

n ul. 

* Jo*; 

DO NOT 

SCALE THIS DRAWING 

— DRAWN 

__ APPftOVEO 

k-L- 

ro* MSC 

9-3-63 

MATERIAL: 


~ &Jj A 

/ a 




JNIT/If. 

APPROVAL 

DATE 




,j/* 

liM 


LIST OF PARTS AND MATERIALS 


REACTOR ASSEMBLY 


CODE IDENT. 




AWG 23 _ SEE N0TE7 

AW G 30 SEE NOTE 5 

_ SEE NO TE'S^ 

_ SEE NOTE 1 

SEE NOTE 6 


SPECIFICATION 















(*) ZONE SYM 

r'Z' A 


_ REVISIONS _ C ~i < ,U _ 

DESCRIPTION P»Tt APPROVAL 

' /!EI//$ED PE.R rpj=trt 05/30 UJhj 

' REVISED PERTDRR 10799 '\T 
' REVISED PERTDRR 11668 afrfa 
'REVISED PERTDRR 15237 


INTERCONNECTIONS 
LI-KSEE NOTE2) 1 L2-I 
LI-3!SEE NOTE 2J L2-3 
LI-5 L2-5 


RED (LI) 
GREEN (L2) —-x, 

r- 


;e nctfs U9 

h- 6.00 MIN — i 
4 LEADS 


-SEE NOTE 10 


.50 DIA 
MAX 


LEAD IDENTIFICATION 
ON SCHEMATIC 1 ON REACTOR" 


LI -1 

LI -2 

LI-3 

LI-4 

LI-6 

L2-2 

L2-4 

L2-6 


RED I 
RED 2 
RED 3 
RED 4 
RED 6 
GREEN 2 
' GREEN 4 
GREEN 6 


SEE NOTE 10- 



-SEE NOTE 7 

STAR] OF .V \L3G 


(jys 

3 PLACES 


6.00MIN ^ .88 MAX- 


6.00 MIN— 


-CD 

<D 

5 Pi AC E- 


WIND! 

NG RESI 

STANCE (REF 

■h 

20% @ 

25 ° C 

FROM 

TO 

OHMS 

LI* 1 

LI-2 

39 

LI* 3 

L 1- 4 

39 

LI- I 

T5T 

39 

LI-3 

L2- 4 

39 

LI-6 

L2-6 

400 

7 

8 

0.02 MAX 

9 

10 

0.02 MAX 


notes: 

1. 

2 . 

3- 


INSULATE BETWEEN REACTORS WITH .002 MYLAR TAPE PER M!^ 1-15126. 

S*E«T L w?NDI« E ®D VI |WPRE6..ANT TO ?50-F. IMPREGNATE WINDING WITH IMPREGNANT. . 

PULL NC VACUUM. BAKE 24 HRS AT 180" F 
WIPE IMPREC-NATiCN DURING CURE CiCLE. 

SET leads equally spaced akcjnd PER! PH FRY OF WINDING,'.'. 'TH MYLmK 
TAPE PER MIL-I-I5I2C-,ORDER OPTIONAL. 

PART N0.I0CI62I MUST EE A MATCHED PAIR. . 

ADD TWO COMMON WINDINGS. ONE {I) TURN EACH. USE WIRE P • v67II-I2,TW0 STRANDS FOR EACH TURN. 
LEAVE 6 INCH WINDING WIRE FOR LEAD. IDENTIFY AS SHO/.... 

THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 1C- MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING 
. ASSEMBLE REACTORS BACK TO BACK 

>. WINDING LEAD “SET END" 

INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
'PRESCRIBED BY MiL-D-70327 


A/R WIRE___ 

A/R AiRE (LEADS) 
A/R IMPREGNANT' 
A/R TAPE_ 


NOMENCLATURE 
OR DESCRIPTION 


1006711-12 
1006711-13' 
1010687- I 


PART OR 
IDENTIFYING NO. 


A WG 2 3 
AW G 3 0 


SPECIFICATION 


SEE N0TE7 
" see NOTE 5 

ill NO TE^4 
SEE NOTE 1 

"see NW 6 ’ 

MATERIAL 
OR NOTES 


NEXT ASSY | USED ON 

APPLICATION 


UNLESS 

OTHERWISE SPECIFIED 

I INSTRUMENTATION LAB 1 

DIMENSIONS 

ARE IN INCHES 

CONTRACT 


TOLERANCES 

ON 

NAS ,5/151 

DATE 

FRACTIONS 

DECIMALS ANGLES 

APPROVED^!* / 




CHECKED /C/ 

9 Jr Yy 



— DRAWN C. y. -V, 

9-9-6? 

DO NOT 

SCALE THIS DRAWING 

APPROVED EUR MSC 


MATERIAL: 


p ( ¥< /a 




irT/IL APPROVAL 

DATE 



M. 

:.vv. 


LIST OF PARTS AND MATERIALS 


REACTOR ASSEMBLY 


UNIT WE I CODE IDENT. 


MIT 

INSTRUMENTATION 
LABORATORY 
_ Cawripor. Maw._ 

owe wo. _ _____ 

MANNED 

SPACECRAFT CENTER 

_ HOUSTON TEXAS 

NASA DRAWING NO. 

1001620 












INTERCONNECTIONS 
LI-KSEE NOTE2)1 L2-l~~~ 
LI-3(SEE NOTE 2) L2-3 

LI-5(SEE NOTE 2) L2-5 


RED(LD- 


GREEN (L2)- 



SEE NOTE I 


6.00 MIN - 
4 LEADS 


.50 DIA 
MAX 


LEAD IDENTIFICATION 
ON SCHEMATIC | ON REACTOR 

Ll-I _ RED I _ 

LI-2 _ RED 2 _ 

LI-3 _ RED 3 _ 

LI-4 _ RED 4 _ 

LI-6 _ RED 6 _ 

L2-2 _ GREEN 2 

L2-4 _ GREEN 4 

L2-6 GREEN 6 


•SEE NOTE 7 

START OF WINDING 


3 PLACES 


6.00 MIN 


6.00MIN I 


.88MAX 


.88 MAX- 


5 PLACES 


-6.00 MIN- 


NOTES: 

1. INSULATE BETWEEN REACTORS WITH .002 MYLAR TAPE PER MIL-1-15126. 

2. BRING OUT ONE LEADWIRE. 

3. PREHEAT WINDING AND HYSOL TO 250’F IMPREGNATE WINDING WITH HYSOL. 

PULL NO VACUM- BAKE 24HRS AT I80*F . . 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. SET LEADS EQUALLY SPACED AROUND PERIPHERY. OF WIND|NG,WITH MYLAR 
, TAPE PER MIL-1-15126, ORDER OPTIONAL. 

6. irPART N0.I00I62I MUST BE A MATCHED PAIR. 

' 7. ADD TWO COMMON WINDINGS.ONE(I)TURN EACH. USE WIRE f^N 10106711-46. 

,' S LEAVE 6 INCH WINDING WIRE FOR LEAD. IDtNTIFY AS SHOWN, 
a THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 500 VOLTS DG AFTER BAKING 



A/R WIRE _ 

A/R WIRE (LEADS) 

A/R HYSOL _ 

A/R TAPE _ 

2 CORE t COIL ASSY 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


1006711-46 
100671H3 
1010687-1 

1001621 1 

PART OR ! 
IDENTIFYING NO. 


SPECIFICATION 


SEE N0TE7 
SEE NOTE 5 " 
SEE NOT E^A 
SEE NOTE 1 
" S£ NOTE 6 

MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M I T 

INSTRUMENTATION LAS 

CONTRACT 

WAS >9^53 TOtE 


\ DNAWM \ /€», V - ~ 

J annnovcd Von MSC 


1000286 I 


LIST OF PARTS AND MATERIALS 


REACTOR ASSEMBLY 


UNIT WT. I CODE IDENT. 


INSTftUM ENT ATION 

LABORATORY 

Canon i oo«. Mann. 

NO. NO 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001620 


APPLICATION 






































































(I 



ZONE SYM 


REVISIONS 

DESCRIPTION 


I DATE I APPROVAL 


VENDING DATA 


TOTAL NUMBER WINDINGS 


TURNS 

AWS' WIRE 
... SI2E . 

TYPE OF 
WINDING 

550 

41 

RANDOM 

550 

41 

RANDOM 

1500 

: 4i ~ 

RANDOM 

COMMON 


WINDING 

RESISTANCE* 


LENGTH SIZE 


IDlNtIF 

START 

I 

3 


AtiOn 

FINISH 

2 

4 


NOTES* 

1. INSULATE BETWEEN WINDINGS NO.I 8 NO.2 WITH A .005 POLYESTER 
WASHER 22 ?d’. PER WIL-l-feil TYPE G. 

2. CORES MUST BE A MATCHED QUAD AND TWO RARTT. 1001621 BE MADE 

3. (■) DENOTES THE SAME INSTANTANEOUS POLARITY. [~ 

4. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. ' 

5. TURNS OR TURNS RATIO TOLERANCE ±1%. I 


SEE NOTE 3 


SCHEMATIC 


WDG 3 
50 0 6 


CORE P 


LJ 

T 2 P) 


CORE 2 


lo 62 36 64 

WDG I WDG 2 



475 DIA 
MAX 


U-435_j 

MAX 

t' nl" «!„ 


Ul/^Ivl.ujJ 


-DIRECTION OP WINDING 
START INSIDE 


A/R POLYESTER 

A/R WIRE _ 

2 CORE _ 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


_ \0Q<oli\-2Z 

_ rOIO€>8B-l __ 

PART OR twruvnifiii 

I IDENTIFYING NO. 

LIST OF PARTS AND MATERIALS 


SEE NOTE I 

SEE DATA 

SEE NOTE 2 

MATERIAL 
OR NOTES 


_ 1000286 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M I T 

•MSTItUMENTATION LAS 

CONTRACT 


APPR OVED *44 

CHECKED 

PRAWN 

APPROVED FOR MSC 


CORE a COIL 
ASSEMBLY 

( REACTOR 
MATCHED PAIR) 


CODE I DENT. 


R1T/IL APPROVAL 


INSTRUMENTATION 
LABORATORY 
Cawriork. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA ORAWINQ HD. 

I00IG2 I 





































































SCALE 


UNIT WT. 


COOE WENT. 


mtstMtsamwmi 

















































































h 


\REV/SED />£* rOKX 05/3 7 


\REV/5ED PER TPRR f/669 


KicmmoN 


25 




r WL* 


telemetry 

OUTPUT 


REF 

DES 

PART NO. 

DESCRIPTION 


T0L 

RATING 

■ftb 

nsnm««i 

RESISTOR 

IK 

HEH 


iiW 

ir«mMFai 



IK 

i% 

Bn 

HEM 

1010695 ! 


SEE NOTE 3 

SAT 

i% 

hezxb 

mrm 

WHJHMM 



SAT 

i% 

win 





499 

■B 

H2ST31 

■M 

IHPEIffEi 



499 

— 

HSECHI 

TM 

IOIC694- 

— 

f see Mote. 5 

SAT 

bqh 

KZEOB 


icm-Bi 

CAPACITOR 

3.3 

M 33 M 

15V 

C2 

rr.ren-f-flE 

CAPACITOR 

3.3 

MMW 

15V 

C3 

1006733-19 

CAPACITOR 

3.3* 

mwdm 

15V 

EB 


DIODE 




VVI 

m&m 

1010497 

I 




_ 

ZZl 


(QQEOi 



!|BI 

bh 

bh 

■B 


BKf 

KSfl 

■ 

- 

□ 

t_ 


L-: 

[_ 


bhi 


bh 



EEE9 

IIQEEEQI 

DIODE 


ihhh 

3.41V 

gUE 

ijggnaHj 

REACTOR ASSY 

\wS 3 m 

ihhh 


Tl 

1001623 

TRANSFORMER 



HBHHI 

R© 

10I03U 


SAT 

\°/o 

MTivrm 



r^*4 'S< tu,& 'm* 


1001622 














































8 


6 


5 



^ r 





D 


C 


B 


A 


R 8 

NOTE 4 
■vW— 



fYYV'i 

« 2 


H. 


0 


K° 

2 ) 


21 ±3V RMS 

32 00 CPS 

SQ. WAVE 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL‘D-70327 

2. UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS 
ALL CAPACITOR VALUES ARE IN UP 

3. R3 K R4 TO BE SELECTED AT TEST 

RANGE OP VALUES FROM 9OK TURU HO K OHMS 

A. R8 (EXTERNAL FEEDBACK RESISTOR.') SELECTED AT TEST 

rauge of Values from 500 oUms thru 7K Q/Vms 

5. F7 T~0 &EL SELLSLCFELD AF F£L 5 7~ 

FtANCrC. of Values from 500 or ms f/Vru /ok oa/ms 


8 


6 


5 


TT 


$ 

3 


-® N 


C? 

3.3 




TELEMETRY 

Output 


\reV/SED PER TPRR//669 


DESCRIPTION 


REV/5ED PER rCPR 05/37 


VCjd 


REV/SED PER TDRK 20730 





REF 

DES 

PART NO. 

DESCRIPTION 

VALUE 

TOL 

RATING 

R1 

.010695-: 26 

RESISTOR 

IK 

1% 

I/8W 

R2 

0.0^5 126 



IK 

IV. 

1/8 W 

R3 

1010^95 


SEE NOTE 3 

SAT 

1% 

1/6 W 

R4 

I0IC695 


SEE NOTE 3 

SAT 

1% 

1/8 W 

R5 

10 0694-97 



499 

1 % 

l/'OW 

R6 

010694-97 



499 

IVo 

1/10 w 

R7 

ICIC 694 - 

... J 

ole Mote 5 

SAT 

1 Vo 

I/IOW 

Cl 

1006 755-19 

CAPACITOR 

3.3 

10 % 

15V 

C2 

1006755-19 

CAPACITOR 

3.3 

10 % 

15V 

C3 

I0C67J5-/9 

CAPACITOR 

3.3 

10 % 

15V 

CRI 

!0',04O7 

DIODE 

500 PIV 


3.4 W 

CR2 

1010497 

_i_ 




j 

CR3 

1010497 




_ 


1 

CR4 

1010497 1 


_ 

i 


* 







CR5 

M04«>7 

DIODE 

500 PIV 


3.4 W 

LI HZ 

10 * IS 20 

REACTOR ASSY 






RtACTOW ' 




Tl 

IOC- IcLd 

TRANSFORMER 




R£ 

I0I03U 

RESlSTCRfSEE NOTE 4 

SAT 

)°/o 

\/;o W 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS AAL IN INCHES 



FRACTIONS DECIMALS ANGLES 






00 NOT SCALE THIS DRAWING 


1000286 

MATERIAL: 

Nt»T ASSY 

UUO ON 


| APPLICATION 



QTY 

NOMENCLATURE 

PART OR 

SPECIFICATION 

MATERIAL 

FINO 

REQO 

OR DESCRIPTION 

IDENTIFYING NO 

OR NOTES 

NO 


LIST OF PARTS AND MATERIALS ] 


i 


£<J'j / 


MSC 

A 'i i l 




SCHEMATIC 

^EATER CURRENT 
AMPLIFIER 


INSTRUMENTATION 

LABORATORY 


ICOI622 














































































































4 


3 


WINDING DATA 


t 






| REVISIONS £> 3 <k < 

ZONE 

SYM I DESCRIPTION 

DATE 


A REVISED PER TDRR 05131 

U-(0-fr3 


APPROVAL 




TOTAL NUMBER WINDINGS 2 


WINDING 

NO. 

TURNS 

TAP 

AT 

AWG WIRE . 
SIZE 

TYPE OF 
WINDING 

WINDINS 
RLSISTdNCLCKEF] 
OHMS t20% @25'C 

LEADS 1 

LENGTH 

SIZE 

IDENTIFICATION 1 

START 

TAP 

FINISH 

PRI 

1000 


41 

RANDOM 

70 

6*' 

30 

1 


2 

SECI 

1200 

600 

41 

RANDOM 

140 

6" 

30 

3 

4 

5 

j 

s 

1 



NOTES: 

1. (■) DENOTES THE SAME INSTANTANEOUS POLARITY 

2. PREHEAT WINDING AND IMPREGNANT TO 250°F. IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM BAKE 24 HRS AT I80°F. 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE ±1%. 

6. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

8. BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A MINIMUM OF 5 DAYS 
PER ND-1002209. CORE MUST MEET PERFORMANCE REQUIREMENTS 

OF SCO 1010689 AFTER TEMPERATURE CYCLING. 


I-1 





























WINDING DATA 


TOTAL NUMBER WINDINGS 2 


WINDING 

NO. 

TURNS 

TAP 

AT 

AWG WIRE 
SIZE 

TYPE OF 
' WINDING 

PRI 

1000 


41 

RANDOM 

SEC 1 

1200 

600 

41 

RANDOM 


_ REVISIONS 

_ DESCRIPTION _ DOTE 

REVISED PER TDRR 05131 IMO-43 

REVISED PER TDRR 06068 t-3H& 


WINDING 


LEADS 


IDENTIFICATION 


notes: 

Ml) DENOTES THE SAME INSTANTANEOUS POLARITY 

2. PREHEAT WINDING AND IMPREGNANT TO 250°F. IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24 HRS AT I80°F. 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE ±1%. 

6. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING 

7. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

8. BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A MINIMUM OF 5 DAYS 
PER ND-1002209. CORE MUST MEET PERFORMANCE REQUIREMENTS 

OF SCO 1010689 AFTER TEMPERATURE CYCLING. 


SEE NOTE I 




SCHEMATIC 

SEC I 
3 4 5 


n ; 

* 2 i 

PRI | 

_*j -25 1 

max r| 


.475 DIA 
MAX 


A/R IMPREGNANT 
MR WIRE (LEADST 

A/R WIRE _ 

I CORE 


NOMENCLATURE 
OR DESCRIPTION 


1010687-1 

I0067IH3 

1006711-22 

1010669-1 

PART OR 
IDENTIFYING NO. 


AWG 3( 
AWG 41 


SPECIFICATION 


NOTE 2^4 
" SEE DATA 
SEE DATA 


MATERIAL 
OR NOTES 


_ 1000286 

iSSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


MIT 

INSTRUMENTATION LAS 

CONTRACT 


LIST OF PARTS AND MATERIALS 

CORE 8 COIL 
ASSEMBLY 

(TRANSFORMER^PWR) 

DALE I UNIT WT. | CODE IOENT. 


liT/IL APPROVAL 


INSTRUMENTATION 

LABORATORY 

' CAWNIP—. MA—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

POI623 

SHEET I OF I 























ZONE SYM 


DESCRIPTION 


MU 


APPROVAL 


WINDING DATA 


TO TAL NUMBER WINDINGS 2 

WINDING T1 , RN<5 TAP AWG WIRE 
NO. TURNS at gZE 

PRI IOOO 41 

SEC I 1200 600 41 


TYPE OF ■ WINDING t- [ | EAD - 

WINDING RESISTANCE LENGTH SIZE 

RANDOM 6" 30 

RANDOM 6" 30 


IDENTIFICATION 
START I TAP I FINISH 
I 2 

3 4 5 


NOTES: 

1. (■) DENOTES THE SAME INSTANTANEOUS POLARITY 

2. PREHEAT WINDING AND HYSOL TO 250°F. IMPREGNATE WINDING 

WITH HYSOL. PULL NO VACUUM. BAKE 24 HRS AT I80°F. 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4. WIPE IMPREGNATION DURING CURE CYCLE. 

5. TURNS OR TURNS RATIO TOLERANCE-± 1%. 

6. THE RESISTANCE BETWEEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 500 VOLTS DC AFTER BAKING 


SEE NOTE I 




SCHEMATIC 

SEC I 
3 4 5 


n 


I 2 
PRI 


.475 DIA 
MAX 



NOMENCLATURE 
OR DESCRIPTION 


1010687-1 I 
1006711-13 
1006711-22 
1010689-1 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


NOTE 24A 
‘ SEE DATA 
SEE DATA 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M I T 

INSTRUMENTATION LAS 

CONTRACT 


1000286 


I approved ^ MSC 


WT/IL approval 


LIST OF PARTS ANO MATERIALS 

CORE a COIL 
ASSEMBLY 

(TRANSFORMER^PWR) 

DALE I UNIT WT. I CODE IDENT. 


INSTRUMENTATION 
LA JURATORY 
‘ Camwion. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWINQ NO. 

1001623 


APPLICATION 


3 


2 





























































3 


2 


REVISIONS 


_ _ REVISIONS _ (*5 _ 

ZONE SYM DESCRIPTION DATE APPROVAL 

A REVISED PER TDRR 05132 n-lt'ti kJtf 



TYPICAL TERMINAL AREA 
SEE NOTE 2 


PRINTED 
CIRCUIT SIDE 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327.. 

2. BOARD CONTAINS (24) .042 DIA HOLES. AS SHOWN ON PR/NtED CIRCUIT PATTER//. 

3. ETCN PATTERN ON BOARD IN ACCORDANCE HIitN PATTERN DRAW/Ng, 1001625. 

4. APOLLO G8N PART NO. 1001624 TO BE STAMPED ON SIDE OF BOARD OPPOSITE PRINTED CIRCUIT 
, PER MH.-STD -130 . 

5. PRINTED - CIRCUIT BOARD PER M/L-P- 5 5 HO. ZlZ-ZZ'rZIZ- 

G>.material: glass clotNEP oxr- res/N lam/Nate pe-ge 03ic i/o 

_L_ . . PER MIL-P-ISJ+JB. 

TSOLDCR COAT .0003 TNlCK MiN. USE sNgO WAUPZ SOLDLE ELE QQ-S-S7L “- 


A/R SOLDER _ 

1 BOARD _ 

/ PRINTED Cl RCU1T PATTERN 


NOMENCLATURE 
OR DESCRIPTION 


1001625 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


NOTE 7 
A/ore a 
REF 

MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 


M I T 

INSTRUMENTATION LAS 


100/618 1000286 
NEXT ASSY USED ON 

APPLICATION 


DIMENSIONS ARE. IN INCHES 

CONTRACT 


TOLERANCES ON 

NAS 9>1J6 

?mr 

FRACTIONS OECIMALS ANGLES 

APPROVED 



CHECKED &/£ 



— DRAWN N. 

9-/C-63 

DO NOT SCALE THIS DRAWING 

__ APPROVED PON MSC 


MATERIAL: 

/AJQ /P/t^ g // 


sec riorc <o 

Mff/iy APPROVAL 

1 DATE 


LIST OF PARTS AND MATERIALS 

BOARD 

PRINTED CIRCUIT 
(heater current 
amplifier) 

SuT - 1 UNIT WT. I CODE IDENT. 


INSTRUMENTATION 

LABORATORY 
Ca»ihipo«, Ma—. 

own. wo. _• 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

IOOI624 

SHEET/ OF/ 


INCHES 


0 I 2 

PHOTOeRAPHKfSCALE ONLY 











































































































































• o/i © 

fol?^roY@)(© 


o)(oX^(oX© 
o)/6) 7o; !o! !ol 




NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
? PRESCRIBED BY MIL-D-70327. 

2. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE 
WITH MIL-STD-440, WITH SN60 WARP2 SOLDER PER QQ-S-571. 

3. UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS* 

ALL CAPACITOR VALUES ARE IN UF. 


1000284 

SSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


00 NOT SCALE THIS DRAWING 
MATERIAL; 



, _ REVISIONS Q ^ _ 

ZONE 1 SYM | DESCRIPTION DATE APPROVAL 

A REVISED PER TDRR 053&3 '2-2 (j)l( 


RESISTOR 

1010695-56 

187 

1/8 W 

RESISTOR 

1010694-130 

UK 

I/IOW 

RESISTOR 

1010694-96 

487 

I/IOW 

RESISTOR 

1010695- 96 

487 

I/8W 

RESISTOR 

1010694-126 

IK 

I/IOW 

DIODE 

1010439 

5.8V 

250 MW 

DIODE 

1010286-2 

IN958B 

400 MW 

CAPACITOR 

1006755-19 

3.3 

15V 

CAPACITOR 

1006755-10 

4.7 

10V 

CAPACITOR 

1006789-4 

56 

8V 

BOARD, PRINTED CIRCUIT 

NOMENCLATURE 

OR DESCRIPTION 

1001544 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 
OR NOTES 


MIT 

INSTRUMENTATION LAB 
CONTRACT 

NAS a-lfia (“DATE 


MSC 

wLU/o-z-l? 

, APPROVAL I DATE 


LIST OF PARTS AND MATERIALS 


PRINTED CIRCUIT 
ASSEMBLY 


SCALE 

NONE 


CODE IDENT. 


INSTRUM ENTATION 
LABORATORY 

tA w mow, Ma—. 

PHWL WO. _ 

MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

~tOO'&2.6~ 

SHEET | OF | 































I r t«j 
i 

i 

| . 

•i" 


] 

I 


i ■ 


'I vj: 2 



i 



notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 

1 PRESCRIBED BY MIL-D-70327. 

2. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE 
WITH MIL-S-6872, WITH SN60WRAP2 SOLDER PER QQ-S-571. 

3. UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS. 

ALL CAPACITOR VALUES ARE IN UF. 


§ 


[ REVISIONS II 

ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL | 


A 

REVISED PER TDRR 053&3 

'2-2<*3 

uM 1 


B 

REVISED PER TDRR 06072 

I-6/-I4- 

"2/ 1 


NEXT ASSY 


1000284 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 
FRACTIONS DECIMALS 


DO NOT SCALE THIS DRAWING 


MATERIAL: 


QTY. 

REQO. 


RESISTOR 


RESISTOR 


RESISTOR 


RESISTOR 


RESISTOR 


DIODE 


DIODE 


CAPACITOR 


CAPACITOR 


CAPACITOR 


BOARD, PRINTED CIRCUIT 


NOMENCLATURE 
OR DESCRIPTION 


M I T 

INSTRUMENTATION LAB 
CONTRACT 


NAS 


p«a»n I V > 


■BaTT 


Vyitil 

T^h 


MSC 


ANDOVIO FOR MS 

IB T/H, APPROVAL [ D 


T7> 


1010695-56 


I0I0694-I3Q 


1010694-96 


1010695- 96 


1010694-126 


1010439-2 


1010286-2 


1006755-19 


1006755-10 


1006789-009 


1001544 


PART OR 
IDENTIFYING NO. 


187 


UK 


487 


487 


IK 


5.8V 


IN958B 


3.3 


4.7 


56 


SPECIFICATION 


1/8 W 


I/IOW 


I/IOW 


I/8W 


I/IOW 


250 MW 


400 MW 


15V 


10V 


8V 


MATERIAL 
OR NOTES 


LIST OF PARTS AND MATERIALS 


PRINTED CIRCUIT 
ASSEMBLY 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


II 


10 


FIND 

NO. 


- - -PTTT- 

INSTRUMENTATION 
LABORATORY 
Camrripor. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 


“TOO\6ser 


SHEET | 


OF | 


a 


I i i i I 


INCHES 

■ I ■ 


PHOTOGRAPHIC SCALE ONLY 


.1 


m 













B 



notes: 

I. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

2 SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE 
WITH MIL-S-6872, WITH SN60WRAP2 SOLDER PER QQ-S-571. 

3 . UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS. 

ALL CAPACITOR VALUES ARE IN UF. 

4. COAT ASSEMBLY' WITH SILICONE RUBBER , PART NO. 1010849, WHEN COMPLETE. 


ZONE 

SYM 

REVISIONS Q 3 f" 

DESCRIPTION 

DATE 

APPROVAL 


A 

REVISED PER TDRR OS3&3 

U-2o<3 



B 

REVISED PER TDRR 06072 

h3/4A- 



c 

REVISED PE/? TDPRE0754 

19 Juu 
... fe5-J 






UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 



FRACTIONS DECIMALS ANGLES 






DO NOT SCALE THIS DRAWING 


10002B4 

MATERIAL: 

NEXT ASSY 

USED ON 


1 APPLICATION 



AR 

SILICONE ROBBER 

1010849 


NOTE 4- 

12 

1 

RESISTOR 

1010695-56 

187 

1/8 W 

II 

2 

RESISTOR 

1010694-130 

I.IK 

I/IOW 

10 

2 

RESISTOR 

1010694-96 

487 

I/IOW 

9 

2 

RESISTOR 

1010695- 96 

487 

1/8 W 

8 

1 

RESISTOR 

1010694-126 

IK 

I/IOW 

7 

1 

DIODE 

1010439-2 

5.8V 

250 MW 

6 

1 

DIODE 

1010286-2 

IN958B 

400 MW _ 

~ 5 

1 

CAPACITOR 

TOO67 55-19 

3.3 

15V_ 

4 

2 

CAPACITOR 

1006755-10 

4.7 

10 V 

" 3 

1 

CAPACITOR __ _ 

1006789-OOS 

56 

8V __J 

2 

1 

BOARD, PRINTED CIRCUIT 

1001544 



1 

QTY. 

REQD. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 


M 1 T 

INSTRUMENTATION 

CONTRACT 

NAS 9-V53 I 

LAS 

DATE 

APPROVED /G GiG/J 

/’ 

CHECKED 

At . 


DRAWN 

e. v v. 


APPROVED FOR MSC 

k) ' /o-Z-& 7 

MftT/IL APPROVAL 

DATE 

W .. , <• l(' 



LIST OF PARjS AND MATERIALS 


PRINTED CIRCUIT 
ASSEMBLY 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


MIT 

INSTRUMENTATION 
LABORATORY 
Camrripqk. Marr. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

\00\*odG 


SHEET | 


OF | 


B 


IOOIG2G C} 

















J 


ill- 


¥ 


■■•‘I 




31 

jf?' 

Ml 


I! 




'hm 

a 


m 

"h II 


!*V‘ 


% 


i 


:■!£ 


4 


M 


' 


t*f\ 


rm; 

* ,? i 




t 



R12 



ZONE 

_L 

SYM 

1 

REVISIONS 0 3 

DESCRIPTION 

DATE 

APPROVAL 


A 

REVISED PER TDRR 053&3 

/2*2o<3 

w~ 


B 

REVISED PER TDRR 06072 




c 

REVISED PE/? TDRR20754- 

i9Jul 

65 



D 

PEI//SED PE/? WPP 2/5/3 

/3/XS6 



C3 


o 




'Pj ! o; 


m 


NOTES: 

1 INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327. 

2 SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE 
WITH MIL-S-6872, WITH SN60WRAP2 SOLDER PER QQ-S-571. 

3 UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS. 

ALL CAPACITOR VALUES ARE IN UF. 

4.COAT ASSEMBLY' WITH SILICONE RUBBER , PART NO. 1010849, WHEN COMPLETE. 


1000284 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M I T 

INSTRUMENTATION LAB 

CONTRACT 


_ NAS 9-V53 

APPROVED 




DATE 


-jJt. 


approved for MSC 

/J )¥#■■' 

my 




flT/IL APPROVAL 


DATE 


U/ u 


AR 

SILICONE RUBBER 

1010849 


NOTE 4- 

12 

1 

RESISTOR 

1010695-56 

187 

1/8 W_ 

IJ 

2 

RESISTOR 

1010694-130 

UK _ 

I/IOW 

10 

2 

RESISTOR 

1010694-96 

487 

I/IOW_ 

9 

2 

RESISTOR 

1010695- 96 

487 

1/8 W_ 

8 


RESISTOR 

1010694-126 

IK 

I/IOW_ 

7 

1 

DIODE 

1010439-2 

5.8V 

250 MW 

6 


DIODE ! 

1010830- 2 _ 

IN958B 

4C0MW 

_5_.. 

1 

CAPACITOR 

I006755-J9 

3.3 1 

i 5 V__ _ 

4 

2 

CAPACITOR 

1006755-10 

4.7 

10 V_ 

3 

1 

CAPACITOR 

I006789-0OS 

56 

8V 

_2_ 

1 

BOARD. PRINTED CIRCUIT 

1001544 



1 

QTY. 

REQD. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO 


LIST OF PAR- 

S AND MATERIALS 

- V MIT 


PRINTED CIRCUIT 
ASSEMBLY 


SCALE 

NONE 


UNIT WT. 


CODE IDENT. 


INSTRUMENTATION 
LABORATORY 
Camrripok. Mam. 


MANNED 

* SPACECRAFT CENTER 

HOUSTON TEXAS 


NASA DRAWING NO. 

\00\<o2.6 


SHEET | 


OF | 


1 




















4 


REVISIONS 


ZONE 


SVM | 


DESCRIPTION 


<9 3^^ _ 

| DATE | APPROVAL 



ST o', io: \o) ipj 


notes: ^ 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. ALL ELECTRICAL CONNECTIONS TO BE MADE WITH SN60 SOLDER 
PER QQ-S-571. 

3. UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN GUMS 
ALL CAPACITOR VALUES ARE IN UF 


REF 

DES 

PART NO. 

DESCRIPTION 

VALUE 

TOL 

RATING 

R3 

1010311 -‘SG 

RESISTOR 

487 

IV. 

I/IOW 

R6 

101031 l - 3G> 


i 

487 


_ 

a 

R7 

ioio3i\-2ae 



IOK 




R8 

1010311 - 130 



I.IK 



V 

R9 

1010311-130 



l!K 



I/IOW 

RIO 

IOI03G4- 112 



187 



I/8W 

Rll 

IOID3G4 - 132 



487 



I/8W 

RI2 

101031 \ - 12G> 



IK 



I/IOW 

RI6 

I0I03G4- 132 

_5 


487 

’ 


I/8W 

RI7 

101031 \-2G5 

RESISTOR 

28K 

\% 

I/IOW 

Cl 

loioeTSS-io 

CAPACITOR 

4.7 

10% 

10V 

C2 

\0\0675f-l0 

—— _ 

4.7 

U 


10V 

C3 

I0I0675T-/9 

T 

3.3 

□ 

L_ 

15V 

C4 

\010675’5-I0 

CAPACITOR 

4.7 

IO*/. 

10V 

CRII 

1010372- 15 

DIODE 

HZ 6544 

5% 

250MW 

CRI2 

1010433 

DIODE 

HZ8683 

5% 

250MW 

1 

IOOI5T44 

BOARQPRMTED CIRCUT1 








UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 

TfH r BA NCES ON 



FRACTIONS DECIMALS ANGLES 





DO NOT SCALE THIS DRAWING 


1000284 

MATERIAL* 

NEXT ASSY 

USED ON 


| APPLICATION 

- 1 


k 


‘I 


d 


c 


QTY. 

REQD. 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


FIND | 
NO. 




MIT 

INSTRUMENTATION LAB 
CONTRACT 

_ 


DATE 

| APPROVED 


CHECKED 



wvvivvfi 

jC' V V- 



J9. msc 




4) 

APPROVAL 

DATE 


%<£\ 

{(,3. 


LIST OF PARTS AND MATERIALS 


PRINTED CIRCUIT 
ASSEMBLY 


SCALE 

NONE 


UNIT WT. 


CODE IOENT. 


1 KTT 

INSTRUMENTATION 

LABORATORY 


SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 


“loo'&as" 


SHEET 


OF 


T 


i'H 


If- 

% A 




Jr# 


r* 


f ■ ; l 














































V $ * » 7 

zone ora I ocschiphow I oatTT 

A REVISED PER TDRR 05124 »1 ^ ' 


REF 

OFS 

PART Na . 

DESCRIPTION 

VALUE 

TOL 

RATING 

Rl 

1010693- 97 

RESISTOR 

499 

1% 

I/4W 

R2 

1010693-97 

RESISTOR 

499 

1% 

I/4W 

R3 

1010693 

RESISTOR 

SEE NOTE 

3 

I/4W 

a 

1006,755-10 

CAPACITOR 

4.7 

10% 

10V 

C2 

1006,755-10 

CAPACITOR 

4.7 

10% 

10V 

CRI 

( 0/0497 

DIODE 

500PIV 


3.4W 

CR2 

( 0/0497 

DIOOE 

500PIV 


3.4W 

CR3 

1010439 

DIODE 

5.8V 

5% 

250mv 

Tl 

T2 

1001629 

TRANSFORMER 

ASSEMBLY 

R«7- 




warn otherwise srcciucp 

DIMENSIONS ARC M RICHES 

TOLERANCES ON 

FRACTIONS DECIMALS MHUI 


00 NOT KAU THU 0RAWIN8 


_ 1000267 

NCXT ASSY USCD ON 

APPLICATION 


OT /y. ARfROVAL DATE 

um 


LIST OF PARTS AND MATERIALS 

SCHEMATIC 

DIAGRAM 

IMU BLOWER CURRENT 
SENSOR 

SCALE I U*T WT. I COOE IOC NT. 


1001627 

SHEET I Of I 

1 , 


























6 



























































T?-‘ 




Ur 


I 



Tl 8 T2-5 


Tl a T2-4 -* 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327, 

2. UNLESS OTHERWISE INDICATED ; 

I AL1_ RESISTOR VALUES ARE \N OHNtS. 

' ALL: CAPACITOR VALUES ARE IN OF 

4. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN - , 

ACCORDANCE WITH MIL-STD-440| WITH SN60 WARP2 

. SOLDER PER QQ-S-571. 

5. JJ5E ATTACHED LEADS 

. ^FOR It/FORMAT/O// RE&ARD/a/h R3 SEE " .. 

LI fJoj~EOfJ DRAH/1*/& /O00287 . 


1000287 


APPLICATION 




$ 


I 


- tf»." Ji* » 




[ REVISIONS | 

ZONE 

SYM 

DESCRIPTION 

DATE APPROVAL 


A 

REVISED PER TDRR 05117 

im»« . (JJi_ 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS OECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


a/r 1 wire 


QTY. 

REQO. 


NOMENCLATURE 
OR DESCRIPTION 


10 0G7\T-13 


PART OR 
IDENTIFYING NO 


AW G 30 


SPECIFICATION 


MATERIAL 
OR NOTES 


FINO 

NO. 


LIST OF PARTS AND MATERIALS 


M 1 T 

INSTRUMENTATION 

CONTRACT 

LAS 

“5XTT 



CHECKED 



DRAWN 

e V. . 7 . 

f-/8-63 

APPROVED PON MSC 

2-f J 

rffr/JL APPROVAL 

DATE 

m 

^3 


WIRING 

ASSEMBLY 


SCALE 


UNIT WT. T CODE IDENT. 


MIT 

INSTRUMENTATION 

LABORATORY 


SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

I00I6Z8 - 


SHEET | 


Of I 


4 








m 

r 

4-i ' 

«*P i ■ »; 

i.l 


i . 

y 




i 


I 


r 


INCHES ' j; 

1,1. I, 1 


» 


p 


l!i‘ 

rl.i 






’ B -• 


, A*1 .!» 


0 I 2 

PHOTOSRAPHHfSCALC ONLY 


I. <?*!■ 

' Itjl. 

I t: 




I Si 

£; *>' 

r r 

- k\ 

VP 

' i?; 

.-■**** 


;s . ■ 
.?• 




p •: > 4 


i- 


it 




























ZONE I SYM 


REVISIONS 

DESCRIPTION 


O^Ot. , 


A REVISED PER TDRR 05117 

B REVISED PER TDRR 11672 


DATE I APPROVAA, 

w tili. 



SEEL NOTE. 5 


NOTES 


i. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 


4. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN 
ACCORDANCE WITH MIL-S-6872 WITH SN60 WRAP2 
SOLDER PER QQ-S-571. 

5. USE ATTACHED UEADS 

<o. FOR It/FORM A T/Of/ RE&ARD///& R3 SEE 
t/OfE Of/ DRAMt*/& 10002.87 




NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


M I T 

INSTRUMENTATION LAS 
CONTRACT 


DO NOT SCALE THIS DRAWING | >q« MS C~ 


1000287 


LIST OF PARTS AND MATERIALS 

WIRING 

ASSEMBLY 

ALE I UNIT WT. I CODE IDENT. 


INSTRUM ENTATION 
LABORATORY 
Camhiook. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001628 


| SHEET | 















1 



notes: 

I. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 
t. UNLESS OTHERWISE INDICATED ; 
j ALU RECTOR VALUE.S ARE OHMS 

: all: capac\tor va\_uee> are kh uf 

3. R3 VALUE. TO BE ‘SELECTED ATTEST 
RANGE OF VALUES FROM 7K OHMS THRU 4 K. OHMS 

4. USE SOLDER SN&O PER QQ-S-571 
. S.DSE ATTACHED LEADS 

-6ZF0M Jf/FOMMATJOf/ ME&AMD/a/(2 M3 SEE 
— d0J~£ Of/ DMAH//A/& JO002.87 




y 






**t 


i 




REVISIONS 

035%<? 



ZONE | SYM | 

DESCRIPTION 

| DATE 

| APPROVAL 


'?1 

■ ;:| 

M- 

> 


IV 

-B! 

-m 


t 



REF 

DES 

PART NO. 

DESCRIPTION 

VALUE 

TOL 

RATING 



Rl 

10\030>3- t<34 

RESISTOR 

499 

V/. 

1/4 W 



R2 

101Q3G3- l®)4 

RESISTOR 

499 

»•/. 

1/4 W 



: R3 

lOlO 3^-3 “““ 

- 

SEE. NOTE 


: i/4 w— 





3 3.A.T. 





: ci 

1006755-/0 

CAPACATOR 

4.7UF 

io% 

: iov 



C2 

7006755-10 

CAP AC ITOR I 

“ 4.7UF1 

10 %. 

IOV 



T1-T2 

iooio>a^ :: 

TRPvYVoFORMER 


. 

:_. 



CRY 

!oro497 

diode. ; . :: : 

urftsz: 

__ - . 

_ 



CRZ 

/o/o49J : 

D\QOE. . : " 

VTR5Z 

. _ _ 



m 

: crs 

IQ1D4*3^ 

: diode.- ::rz:: 

HZB8B3: 


: 230MW 


1 


U 



rm \ 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


NEXT ASSY 


1000287 

USED ON 


APPLICATION 


DO NOT SCALE THIS DRAWING 


MATERIAL: 


A/R [WIRE 


QTY. 

REQO. 


I0I0G7U-13 


NOMENCLATURE 
OR DESCRIPTION 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


NO. 


M 1 T 

INSTRUMENTATION 

CONTRACT 

_!UAS^153J 

LAB 

"5aTT 

APPROVED > 


/o-7-C\ 

CMECFCD 

zk 

9U+3 

DRAWN 

e. j. j. 

1-/6-63 

APPNOVCO FOR MSC 

4J(1 

1-C3 

Ml /JL APPROVAL 

DATE 

vOc 



LIST OF PARTS AND MATERIALS 


WIRING 

ASSEMBLY 


SCALE 


UNIT WT. I CODE IDENT. 


-ETTT- 

INSTRUM ENT ATtON 
LABORATORY 


SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWINQ NO. 


1001628 


SHEET 


s. \ 

!L 


i 


I. 

p 

,?- - ; 





























































REVISIONS 


__ 035~4 

ZONE SYM _ DESCRIPTION _ DOTE | 

A REVISED PER TDRR 05118 \lio-bl\ 


LEAD IDENTIFICATION 
ON SCHEMATIC I on REACTOR 
Tl-I RED I 

TI-2 RED 2 

TI-3 RED 3 

T2-I GREEN I 

T2-2 GREEN 2 

T2-3 GREEN 3 


WINDING RESISTANCE (REF) 
±20%(o) 25 0 C 


START 

CE 

RED(TO 


FROM 

TO 

OHMS 

Tl-I 

TI-2 

22.5 

TI-2 

TI-3 

22.5 

T2-I 

T2 —2 

22.5 

T2-2 

T2-3 

22.5 

4 

5 

.02 MAX 



GREEN (T2) 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. MAKE LEADS 6 IN. LG., USE WIRE PER FART N0.I0 067IH3. SET LEADS EQUALLY 

SPACED AROUND PERIPHERY OF WINDING,ORDER OPTIONAL,WITH MYLAR TAPE PER MIL-1-15126 
• 3. PREHEAT WINDING AND IMPREGNANT TO 250°F. IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24 HRS. 

AT 180 °F. 

4 . ADD COMMON WINDING I TURN OF W'PF PART NO. 1006711-46 
LEAVE 6 IN. WINDING WIRE FOR LEAj. , U u . 'IFY AS SHOWN. 

5.INSULATE BETWEEN WINDINGS WITH .002 MYLAR TAPE. PER MIL-M5I26. 

6. WIPE IMPREGNATION DURING CURE CYCLE 

7 THE RESISTANCE BETWEEN WNDNGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING 


A/R TAPE _ 

A/R I WIRE (LEAD S) 
A/RI IMPREGNANT 
A/^~ WIRE _ 

2 TRANSFORMER 


NOMENCLATURE 
OR DESCRIPTION 


10 0G7H-I3 
1010687-1 
1006711-46 
1001630 

PART OR 
IDENTIFYING NO. 


AW 6 30 


AW6 20 


SPECIFICATION 


5EN0TE2C5 
SEE NOTE 2 ~ 
SEE NOTE 3£6" 
SEE NOTE 4 ’ 


MATERIAL 
OR NOTES 


_ 1000287 

SSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M I T 

INSTRUMENTATION LAS 

CONTRACT 


LIST OF PARTS AND MATERIALS 


TRANSFORMER 

ASSEMBLY 


CODE IDENT. 


SIT/IL APPROVAL 
—’ 


INSTRUMENTATION 
LABORATORY 
Cawripoe. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001629 

SHEET I OF I 



































3 


2 


1 


_ REVISIONS Q3 S’il 

_ DESCRIPTION _ DATE 

REVISED PER TDRR 05118 il-it-tt 
REVISED PER TDRR 06069 


LEAD IDENTIFICATION 
ON SCHEMATIC I ON REACTOR 
Tl-I RED I 


TI-2 

TI-3 

T2-I 

T2-2 

T2-3 


RED I 
RED 2 
RED 3 
GREEN I 
GREEN 2 
GREEN 3 


WINDING RESISTANCE (REF) 


START 

(E 

RED (TIJ 


±20%<’ 

a 25°c 


FROM 

TO 

OHMS 

Tl-I 

TI-2 

22.5 

TI-2 

TI-3 

22.5 

T2-I 

T2-2 

22.5 

T2-2 

T2-3 

22.5 

4 

5 

.02 MAX 



GREEN (T2) 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. MAKE LEADS 6 IN. LG., USE WIRE PER FART N0.I0 067IH3. SET LEADS EQUALLY 

SPACED AROUND PERIPHERY OF WINDING,ORDER OPTIONAL,WITH MYLAR TAPE PER MIL-1-15126 

3. PREHEAT WINDING AND IMPREGNANT- TO 250°F. IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24 HRS. 

• AT 180 # F. 

4 . ADD COMMON WINDING.2 TURNS OF WIRE PART NO. 1006711-46. 

LEAVE 6 IN.WINDING WIRE FOR LEAD. IDENTIFY AS SHOWN. 

5.INSULATE BETWEEN WINDINGS WITH .002 MYLAR TAPE. PER MIL-115126. 

6. WIPE IMPREGNATION DURING CURE CYCLE: 

7 THE RESISTANCE BETWEEN WNDMGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING - 


A/R TAPE 

A/R WIRE (LEADS) 

A/R IMPREGNANT 

WIRE _ 

2 TRANSFORMER 


NOMENCLATURE 
OR DESCRIPTION 


10 06711-13 
1010687-1 
1006711-46 
1001630 

PART OR 
IDENTIFYING NO. 


AW 6 30 


AW6 20 


SPECIFICATION 


SEEN0TE2f5 5 
SEE NOTE ? 4 
" SEENOTE3& 3 
SEE NOTE 4 2 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 


MIT 

INSTRUMENTATION LAR 


_ 1000287 

SSY USED ON 

APPLICATION 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 

APPROVED 

CONTRACT 

mm 

“5aTF 



CHECKED 


93c-£ 

DO NOT SCALE THIS 

DRAWING 

— DRAWN 

APPROVED 

"* MS* 

i 

MATERIAL: 







| <flT^IL APPROVAL | 

DATE 




Tzrrn 



LIST OF PARTS AND MATERIALS 


TRANSFORMER 

ASSEMBLY 


CODE IDENT. 


INSTRUMENTATION 

laboratory 

Ca—« t«oo«, Ma—, 


MANNED 

SPACECRAFT center 

HO^TDN TEXAS 
ItftA DRAWING NO. 

1001629 

SHEET I OF | 


INCHES 


0 I 2 

PHOTOGRAPHIC SCALE ONLY 
















ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 


A 

REVISED PER TDRR 05118 

12*0-65 

ud— 


B 

REVISED PER TDRR 06069 




c 

REVISED PER TDRR 10798 

IS JOL 

„ 4*-. 



, LEAD IDENTIFICATION | 

ON SCHEMATIC 

ON REACTOR 

Tl-I 

RED 1 

TI-2 

RED 2 

TI-3 

RED 3 

T2-I 

GREEN 1 

T2-2 

GREEN 2 

T2-3 

GREEN 3 


WINDING RESISTANCE (REF) 
±20% (a) 25°C 

FROM 

TO 

OHMS 

Tl-I 

TI-2 

22.5 

TI-2 

TI-3 

22.5 

T2-I 

T2 — 2 

22.5 

T2-2 

T2-3 

22.5 

4 

5 

.02 MAX 



notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. MAKE LEADS 6 IN. LG., USE WIRE PER PART N0.IOO67IH3. SET LEADS EQUALLY 

SPACED AROUNO PERIPHERY OF WINDING,ORDER OPT!ONAL,WITH MYLAR TAPE PER MIL-1-15126 

3. PREHEAT WINDING AND IMPREQNANT TO 250°F. IMPREGNATE WINDING 
WITH IMPREGNANT. PULL NO VACUUM. BAKE 24 HRS. 

AT 180° F. 

4. ADD COMMON WINDING.2 TURNS OF WIRE PART NO. 100671 1-I2,TW0 STRANDS FOR EACH TURN. 
LEAVE 6 IN.WINDING WIRE FOR LEAD. IDENTIFY AS SHOWN. 

5.INSULATE BETWEEN WINDINGS WITH .002 MYLAR TAPE. PER MIL-115126: 

6. WIPE IMPREGNATION DURING CURE CYCLE. 

7 THE RESISTANCE BrT'WFEN WINDINGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 250 VOLTS DC AFTER BAKING 


ML 

A/h 

-, /r 
vs 

IAPE 



SENOTE2C5 

5 

ITVi RE (LEADS) 

iO 06711-13 

AWG 30 

S-t NOTE 2 

4 

IMPREGNANT 

V\ IhE 

i 010687-1 


SEE NOTE yjo 

3 

100671 1-1 £ 

AWG 23 

Shi NOTE 4 

2 

2 

TRANSFORMER 

1001630 



1 

QTY. 

REQD. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 


LIST OF PARTS AND MATERIALS 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 



FRACTIONS DECIMALS ANGLES 






DO NOT SCALE THIS DRAWING 


1000287 

MATERIAL: 

NEXT ASSY 

USED ON 



M ! T 

INSTRUM ENT ATION 
LABORATORY 

_Cammidw, Maw. 


M I T 

INSTRUMENTATION LAS 

CONTRACT 

NAS, 9, 

7? 






DATE 






MSC 


IT/IL APPROVAL 




WZi 


TRANSFORMER 

ASSEMBLY 


SCALE 


UNIT WT. I CODE IDENT. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 


IOOI&29 


SHEET I 


OF 


APPLICATION 






















LEAD IDENTIFICATION 
ON SCHEMATIC 1 ON REACTOR 

Tl-I RED I 

TI-2 RED 2 

TI-3 RED 3 

T2-I GREEN I 

T2-2 GREEN 2 

T2-3 GREEN 3 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. MAKE LEADS 6 IN. LG.,USE WIRE PER RART N0.I0I067IH3. SET LEADS EQUALLY 

SPACED AROUND PERIPHERY OF WINDING,ORDER OPTlONAL.WlTH MYLAR TAPE PER Mll-I-15126 

3. PREHEAT WINDING AND HYSOL TO 250°F. IMPREGNATE 

WINDING WITH HYSOL. PULL NOVAGJM. BAKE 24 HOURS 

AT 180° F. 

4. ADD COMMON WINDING I TURN OF WIRE PART NO. 1006711-46 
LEAVE 6 IN. WINDING WIRE FOR LEAD. IDENTIFY AS SHOWN. 

5.INSULATE BETWEEN WINDINGS WITH .002 MYLAR TAPE. PER MIL-I-I5I26. 

6. WIPE IMPREGNATION DURING CURE CYCLE. 

7 THE RESISTANCE BETWEEN WMDNGS SHALL NOT BE LESS THAN 10 MEGOHMS 
WHEN MEASURED AT 500 VOLTS DC AFTER BAKING ' 


A/R TAPE _ 

A/R WIRE (LEADS). 

A/R HYSOL 

a7^~ WIRE _ 

2 TRANSFORMER 


NOMENCLATURE 
OR DESCRIPTION 


10106711-13 

1010687-1 

1006711-46 

1001630 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


SEEN0TE2C5 
' SEE NOTE2 
SEE NOTE 3^6" 
" SEE NOTE 4 " 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANOLCS 


DO NOT SCALE THIS DRAWING 


1000287 


MIT 

INSTRUMENTATION U| 
CONTRACT 

NAS,9/453 roSTT 


■IT/IL APPROVAL 


LIST OF PARTS AND MATERIALS 


TRANSFORMER 

ASSEMBLY 


COOE I DENT. 


INSTRUMENTATION 

LABORATORY 
Camppippp. mass. 


MANNEO 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWINQ NO. 

IOOI629 


APPLICATION 

























































| REVISIONS 03 5^? 

ZONE 

SYM 

DESCRIPTION | 

DATE 

APPROVAL 


A 

REVISED PER TDRR 05119 

iz-/a-*s 

id# 


WINDING DATA 


TOTAL NUMBER WINDINGS 1 


WINDING 

NO. 

TURNS 

AWG WIRE 
SIZE _ 

TYPE OF 
WINDING 

LEADS 

WINDING 

RESISTANCE REF 
0HMS±20% (© 25°C 

LENGTH 

SIZE 

IDENTIFICATION 

START 

CT 

FINISH 

1 

500 

36 

BIF1LAR 

6“ 

SAME 
AS WDG 

1 

2 

3 

45 


notes: 

L DIRECT\ON OF WINDING STARTS TN6IDE 

2. SET LEADS EQUALLY SPACED AROUND PERIPHERY OF WINDING. 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4 . TURNS OR TURNS RATIO TOLERANCE ±1%. 

5. (») DENOTES THE SAME INSTANTANEOUS POLARITY _ 

6. BEFORE WINDING, TEMPERATURE CYCLE CORES FOR A | 
MINIMUM OF 5 DAYS PER ND-f002209 CORE MUST 
MEET PERFORMANCE REQUIREMENTS OF SCD-I0I0696 
AFTER TEMPERATURE CYCLING. 

7. INTERPRET DRAWING IN ACCORDANCE WITH 
STANDARDS PRESCRIBED BY MlL-D-70327. 


SEE NOTE 



SEE NOTE I 


Ai/R 

wire 

I00G7U-20 

A WG 33 

SEE DATA 

2 

\ 

CORE ':.— 

\O\0k9b-l 



V 

QTY. 

REQO. 

NOMENCLATURE 

OR DESCRIPTION 

PART OR 
IDENTIFYING NO. 

SPECIFICATION 

MATERIAL 

OR NOTES 

FIND 

NO. 


LIST OF PARTS AND MATERIALS 


/ oo/6as 


1000287 


APPLICATION 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


M I T 

INSTRUMENTATION LAB 
CONTRACT 

AS 9,15 


DO NOT SCALE THIS DRAWING 



CORE a COIL 
ASSEMBLY 
(TRANSFORMER) 


UNIT WT. 


CODE IDENT. 


M IY 

INSTRUM ENTATION 
LABORATORY 

CAMRRIOOK. MA—. 


SPACECRAFT CENTER 
HOUSTON TEXAS 


NASA DRAWING NO. 

1001630 


SHEET / 


OF/ 


♦sar'Sfe.V a ?-,.***: : 


INCHES 

I ■ 1 * l«t i 

0 I 2 

i PH OTOGRAPHKf SCALE ONLY 
































ZONE I SYM 


REVISIONS QZS(s\ 
DESCRIPTION 


DATE I APPROVAL 


WINDING DATA 


TOTAL NUMBER WINDINGS l 


WINDING 

NO. 


TURN5~ 

AWG WIRE 
SIZE _ 

TYPE. OF 
WINDING 

500 

36 

BIF1LAR 


LEADS _ 

|_I IDENTIFICATION 


START CT FINISH 


SAME 
AS WDG 



notes: 

L DIRECTION OF WINDING STARTS \NS1DE 

2. SET LEADS EOUALLY SPACED AROUND PERIPHERY OF WINDING. 

3. WIND WINDINGS OVER ENTIRE LENGTH OF CORE. 

4 . TURNS OR TURNS RATIO TOLERANCE ±1%. 

5. (■) DENOTES THE SAME INSTANTANEOUS POLARITY _ 

RESISrAf/CE BErh/£Ej/ nZ/f/D/AiaS sdiLL ' 

TZ A/Or BE LESS T//aa/ 10 MEOod*fS H/Ze// j 

_ MEASURED AT 500 VDC . Z . 


SEE NOTE 5 


SCHEMATIC 

2 3 

T 500? 


65 DIA 
MAX 



TT 


- 


-SEE NOTE I 


I 

i 

i 

5 


A/R WIRE 

I CORE 


IOOG7H-2Q 
\°\0 kSb-i 


NOMENCLATURE 
OR DESCRIPTION 


I | IDENTIFYING* NO. j •^BFICATION 

LIST OF PARTS AND MATERIALS 


SEE DMA 


MATERIAL 
OR NOTES 


_ 1000287 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS APE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


00 NOT SCALE THIS DRAWING 
MATERIAL: 


M I T 

INSTRUMENTATION LAS 
CONTRACT 

NAS. 9,133 ["date 

A "« ovtD feicL 

CHtc «f°. jktEmZ %'Js* 

drawn p -/ y, 

APPROVED FOR MSC 


CORE a COIL 
ASSEMBLY 
(TRANSFORMER) 


CODE ident. 


INSTRUM ENTATION 
LABORATORY 
Cam—idm. Ma—. 

DM. MO. _ 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

IOQ163Q~ 

SHEET OF 

































































REVISIONS 0 35 (* 9 


I ZONE I SYM 


DESCRIPTION 


DATE I APPROVAL 


[A \/?£l//5£D />£/? ran# of/20 1 / 2-443 [ 


SEE NOTE 3 
2 PLACES 



SEE NOTE 2 


kD 


2 PLACES 


NOTES: 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL*D-70327 

2. SURFACE TO BE FLAT WITHIN .015 TLR.. 

3. BRAZE PER MIL-B-7883. WITH CLASS 4 SILVER SOLDER PER QQ-S*5GI 

4. FINISH - TIN PLATE PER MIL-T-10727 TYPE U (HOT DIP). 

5. PAN HD. SCREW,CRES, N0.4-40NC-2A LG. PER. MS 35233-14. 


CASE-MACHINED 

SCREW 


NOMENCLATURE 
OR DESCRIPTION 


1001634 


PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS 0EC1MALS ANGLES 


DO NOT SCALE THIS DRAWING 


1000287 


MIT 

INSTRUMENTATION LAS 
CONTRACT 

NAS /9>4S3 fDATE 


llT/f APPROVAL 


LIST OF PARTS AND MATERIALS 


CASE ASSEMBLY 


UNIT WT. 


CODE IDENT. 


INSTRUMENTATION 

LABORATORY 

Cammiom, Mars. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

300IGSI : 


APPLICATION 



PHOTOe«APHHf8CALE ONLY 






























notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. SURFACE TO BE FLAT WITHIN .015 TLR.. 

3. BRAZE PER MIL-B-7883. 

4. FINISH-TIN PLATE PER MIL-T-10727 TYPE H (HOT DIP). 

5. PAN HD. SCREW,CRES, N0.4-40NC-2A *f£LG. PER MS 35233-14. 












































ZONE SYM 


DESCRIPTION 


DATE I APPROVA 


A \/t£W5£D P£* TOSH 05/2, / W-+U 


2X3)4 PLACES 


2 4 

© © 

© © 

13 



-.5—Hh-~.040MAX 

MiN 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED 
I BY MIL-D- 70327 

2. SOLDERING PER MIL-S-6872A WITH SN50WARP2 SOLDER 
1 PER QQ-S-571 


A/R SOLDER _ 

4 TERMINAL _ 

I COVER-MACHINED 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


f [010690-1 
1001633 

PART OR 
IDENTIFYING NO. 


SEE MOTE 2 3 

_2_ 

i 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DC NOT SCALE THIS DRAWING 


MIT 

INSTRUMENTATION LAS 

CONTRACT 


1000287 


LIST OF PARTS AND MATERIALS 


COVER ASSEMBLY 


CODE IDENT. 


IfT/IL APPROVAL 


INSTRUM ENTATION 
LABORATORY 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001632 


APPLICATION 


.r* 































2 4 

© 0 

© © 

I 3 



2X3) 4 PLACES 



.040 MAX 


I. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 
.2. SOLDER WITH SN50 PER QQ-S-571 ' - - 


A/R SOLDER _ 

4 TERMINAL _ 

I COVER-MACHINED 

QTY. NOMENCLATURE 

REQO. OR DESCRIPTION 


r 1010690'-1 

1Q01G33 

PART OR 
IOENTIFYINO NO. 


SPECIFICATION 


1SEE M0H2J 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MIT 

WMTftUMENTATION LAG 
CONTRACT 


1000287 ] 


LIST OF PARTS AND MATERIALS 


COVER ASSEMBLY 


CODE IDENT. 


IfT/M. APPROVAL 


INSTRUMENTATION 

LABORATORY 


MANNED 

SPACECRAFT CENTER 

HOUSTON TEXAS 
NASA DRAWING NO. 

IOOIG.32 ' 


APPLICATION 


























































2 


REVISIONS _03£4t 

DESCRIPTION I I 


Of ZONE SYM _ DESCRIPTION _ 

„ A REVISED PSA roAX 04-53! ih^3 


DATE I APPROVAL 


» - 119 
" .099 

TYP 



.22 L .421, 

.20 . 39 r 


SEE NOTES 2 8 3 


2 PLACES 


133 ± g0| D|A T hru 4 PLACES 



rtia +.002 
,019 -.003 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

3. ENGRAVE OR METAL STAMP PER ND 1002010 (.09 CHARACTERS), 

4. FINISH-TIN PLATE PER MIL-T-10727 TYPED (HOT DIP). 


5.BRE.AW ALL SHARP EDGES .010 MAX. 


I [COVER. RECTANGULAR 


NOMENCLATURE 
OR DESCRIPTION 


I io/oef/-4^ 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M I T 

IN ST R UMENTATION LAS 

COMTIMCT 


1000287 


LIST OF PARTS AND MATERIALS 


COVER-MACHINED 


coot I DENT. 


T/IL APPROVAL 


APPLICATION 



INSTRUMENTATION 
LABORATORY 
Camsridss* mass* 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

(00I&33 

































































REVISIONS 


01SU 


REVISED PER TOR* 04-53! 

' REVISED PER TDRR 05122 It-it-U 



notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

3. ENGRAVE OR METAL STAMP PER ND 1002010 8 ND1002122, TYPE H, CLASS I, .09 CHARACTERS. 

4. FINISH-TIN PLATE PER MIL-T-10727 TYPE II (HOT DIP). 


5. BREAK ALL SHARP EDGES .0\0 MAX. 











































4 





, .119 
* .099 
TYP 



SEE NOTES 2 a 3 


2 PLACES 


.120 + DIA THRU 4 PLACES 



rtlo +.002 

.019 -.003 



MX) 


notes: 


1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. CHARACTERS TO BE CENTERED ON RESPECTIVE CENTER LINES. 

3. ENGRAVE OR METAL STAMP PER ND 100201<3 (.09 CHARACTERS), 

4. FINISH-TIN PLATE PER MIL-T-10727 TYPED (HOT DIP). 


5. BREA.* ALL SHARP E.DGE.S .010 MAX. 


I 1 COVER. RECTANGULAR 


NOMENCLATURE 
OR DESCRIPTION 


/Q/067/-4 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MIT 

INSTRUMENTATION LAS 

CONTRACT 


1000207 


LIST OF PARTS AND MATERIALS 


COVER-MACHINED 


CODE I DENT. 


RlT/IL APPROVAL 


INSTRUMENTATION 
LABORATORY 
Cammiom. Mam. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

100T&33 


APPLICATION 


3 


































































3 


2 


REVISIONS 




ZONE SYM 


DATE APPRO 


REVISED PER TDRR 05123 



.M3 IqoI DIA THRU 
Z HOLES 


870 REF 


.26 « .567 
.24 ** .557 


■1.063 REF 



.719 REF 


•51DIA THRU 

.49 


1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED BY MIL-D-70327. 

2 . break all sharp edges .oio max .i.'.v 


|CASE,RECTANGUL4R 


NOMENCLATURE 
OR DESCRIPTION 


IO\OGS\ -3 

PART OR 
IOENTIFYINQ NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


MIT 

INSTRUMENTATION LAS 
CONTRACT 


1001631 11000287 | material: 


APPLICATION 


flr/l L APPROVAL 


LIST OF PARTS AND MATERIALS 


CASE-MACHINED 


CODE IDENT. 


INSTRUMENTATION 

LABORATORY 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 


I00IGS4 


INCHES 


PH 0T08RAPHI<f SCALE ONLY 



























3 


2 



.M3 iSg OIA THRU 
Z HOLES 


.915 MAX 


.26 L .567 
.24 M .557 


-1.09 MAX 



.75 MAX 



•51 DIA THRU 
.49 


NOTE 


1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. BREAK ALL SHARP EDGES .OlO MAX - 


| CASE, RECTANGULAR 


NOMENCLATURE 
OR DESCRIPTION 


1010631 -3 

PART OR 
IOCNTIFYINQ NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


M IT 

INST R UMENTATION LAG 
CONTRACT 


I APPROVED TOR- MSC 


1000287 


LIST OF PARTS AND MATERIALS 


CASE-MACHINED 


CODE IDENT. 


INSTRUMENTATION 

LABORATORY 
Cawrripor. Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 


1001634 


APPLICATION 


3 




















































■rv/ieirtkiC 


REDUCE 4!l TO 1.000 ±.005 ••J 
_ PHOTO REF__ 




REDUCE 
4*.l TO 1.000 
±.005 
PWOTO REF 



PART OR 
IDENTIFYING NO. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


■ 

! 


UNLESS OTHERWISE SPECIFIED M 1 T 

Ar%r lu/Hjee INSTRUMENTATION LAS 

DIMENSIONS ARE IN INCHES cammidm, mam. 

TOLERANCES ON - coutiuct 

FRACTIONS DECIMALS ANGLES qpawn V. V. DATE *-'*"* 

* ± * rMFCKFn j 

DO NOT SCALE THIS DRAWING appphu ai 

MATFRIAl * *«—*,*, 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 

PRINTED CIRCUIT 
PATTERN 


1000284 


I HEAT TREATMENT 


USED ON | FINAL FINISH 


APPLICATION 


NASA APPROVAL. 


MIT APPROVAL. 


V/O 


xtogt* 


I CODE IOENT NO. SIZE 


SCALE 4/1 I WT 


NASA DRAWING NO. 


1001635 







































































3 


REVISIONS 



L2-4-* 
SEE NOTE 3 


» L2-5 
SEE NOTE 3 


L2-2-* 
SEE NOTE 3 


L2-REF- 


•L2t7" 

I SEE NOTE 3 


esl \ct6\ \c*r\ \c*a\ 


TERMINAL-7 


•LI-12 SEE NOTE 3 

• L2-I2 SEE NOTE 3 
TI-7 SEE NOTE 3 

• TERMINALS 0 5 9. 
LI-9 SEE NOTE 3 

•L2-9 SEE NOTE 3 


R7 

SEE NOTE 4 


TI-IO - - 

SEE NOTE 3 


Tl-4-s-^ 

SEE NOTE 3 


L2-I3 -» 
SEE NOTE 3 
LI-REF—^ 


LI-2 

SEE NOTE 3 


L2-I4 
SEE NOTE 

Hi 3 


C*/\ toe* lorsl \C£4\ 


■TI-REF 


TI-6 SEE NOTE 3 


•TI-8 SEE NOTE 3 
SEE NOTE 3 


LI-7 

SEE NOTE 3 


LI-4-* 
SEE NOTE 3 


•LI-5 

SEE NOTE 3 


notes: 

1. INTERPRET OR AWING IN ACCORDANCE WITH STANDARDS • 

2 PRESCRIBED BY MIL-D-70327. 

2. SOLDERING OF ELECTRICAL CONNECTIONS TO BE IN ACCORDANCE 
WITH MIL-STD-440, WITH SN60 WARP2 SOLDER PER QQ-S-571. _ 

3. USE ATTACHED LEAD. 

4. FOR INFORMATION REGARDING R4,R5,R7,RI3.RI4,.5 RI5 SEE 
NOTES ON DRAWING 1000284. 


UNLESS OTHERWISE SPECIFIED 
DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGUS 
* * ± 

DO NOT SCALE THIS DRAWING 


REVISED PER TDRR 0S3(>5 


ADDITIONAL 

CONNECTIONS 


LI-I.LI-6 
LI-3, LI-8 
L2-I.L2-6 
L2-3.L2-8 

Tl-I _ 

TI-2 

LM6 

LI-1 7 .- .. 

LI-10 

LI-11 

L2-I0 

L2-II 

LI-14 

LI- 13 

LI-15 

LI-18_ 


A/R 1006711-13 


TI-5 _ 

TI-3 _ 

Tl-ll _ 

TI-9 

TERMINAL I 
T ERMINAL 2 
TERMINAL 3 
TERMINAL 10 

R4 

R5 

RI4 _ 

RI5 _ 

TERMINAL 6 
TERMINAL 5 
TERMINAL4 
R7 


WIRE AWG 30 


PART OR 
IDENTIFYING NO. 


M I T 

INSTRUMENTATION LAS 
Cammimc. Maw. 


NOMENCLATURE OR 
DESCRIPTION 


LIST OF MATERIALS 


MANNED SPACECRAFT CENTER 

HOUSTON, TEXAS 


WIRING ASSEMBLY 


1000284 


I HEAT TREATMENT 


I FINAL FINISH 


APPLICATION 


[NASA APPROVAL 4yQ- 


I MIT APPROVAL 


CODE IDENT NO. SIZE 


NASA DRAWING NO. 



C 1001636 


| SCALE 2/1 I WT 


I SHEET I OF I 


>lQlc; 











































































































































































































































INTERCONNECTIONS 
L3-lfeEE NOTE 2) 1 L4-I 
L3-3(SEE NOTE 2) L4-3 
L3-7CSEE NOTE Z) L4-7 

L3-6 _ L4-6 

L3-IO_L4-I0 


GREEN (L4) 


RED(L3) 


13 PLACES) 


.50 DIA MAX 


LEAD IDENTIFICATION 
ON SCHEMATIC I ON REACTOR - 


BEE NOTE 4(2 



■6.00 MIN - 
13 WIRES 


L3-I 

L3-2 

L3-3 

L3-4 

L3-5 

L3-7 

L3-9 

L4-2 

L4-4 

L4-5 

L4-9 

L3-8 

L4-8 


RED I 
RED 2 
RED 3 
RED 4 
RED 5 
RED 7 
RED 9 
GRN 2 
GRN 4 
GRN 5 
GRN 9 
RED 8 
I GRN 8 


notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. BRING OUT ONE LEADWIRE. 

3.SET LEADS EQUALLY SPACED AROUND PERIPHERY OF WINDING. 
ORDE.R OPTIONAL, USE. MYLAR TAPE PER. MIL- I - 1512.G 

4. INSULATE BETWEEN WINDING WITH .002. NYLON TAPE PER MIL-1* 15126 

5. WIPE IMPREGNATION DURING CURE.” CYCLE. 

£. PREHEAT WINDING AND HYSOi- TO 2.50* F, IMPREGNATE WINDING 
L WITH HYSOL..PULL NO VACUUM. BAKE 2.4 HRS AT ISO’F 
T PART NO. IOOISAO MUST BE MATCHED PAIR 

g. t/Je res/s taa/ce betiVee// wu/dj, fes sj/alL t/or be less iztzziiz:- 

E17^A// JO MEGOf/MS AT 500 VDC AETER BAKING 





A/R WIRE (LEADS') " 
A/R HYSOL 
A/R TAPE 

a core a coil assy 


NOMENCLATURE 
OR DESCRIPTION 


100G7U-13 
1010GB7- \ 

1001540 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


SEE NOTE 5 
SEE NOTE 
" SEE NOTE 4 
' DENOTE 7 

MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


DO NOT SCALE THIS DRAWING 


100028^ 


M i T 

•NGTftUMCNTATION LAN 

CONTRACT 

NAS A453 rwff 


MSC 

jt //)— 2—C 


LIST OF PARTS AND MATERIALS 

REACTOR ASSEMBLY 

(second stage) 

Scale I unit wt. I code ioent. 


APPLICATION 


MIT/1L APPROVAL 

U 


INSTRUMENTATION 
LA MORATORY 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 


1001638 





























































■KU1 












.*4 




! 










jt aS ai jj i s i Zu/as sS & 

MIS' 





1.026 

1.012 




" 0IA-THRU 

16 HOLES ON .203 PITCH BSC 
SPACED AS SHOWN 

|& .015 DIAl 


in 


u!5& REF 


-.019 REF 



notes: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. FINISH-TIN PLATE PER MIL-T-10727 TYPE H (HOT DIP) 

3. BREAK ALL SHARP EDGES .010 MAX 


V COVER, RECTANGULAR 


NOMENCLATURE 
OR DESCRIPTION 


1010G91-4 

PART OR 
IDENTIFYING NO. 


SPECIFICATION 


MATERIAL 
OR NOTES 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


00 NOT SCALE THIS DRAWING 


M I T 

INSTRUMENTATION LAB 

CONTRACT 


1 DRAWN l/f. VW. 

APPAOVtO to* J*SC 


LIST OF PARTS AND MATERIALS 


COVER-MACHINED 


1000283 


UNIT WT. 


COOE IDENT. 


APPLICATION 


ifr/llj APPROVAL 




INSTRUM ENTATION 
LABORATORY 
Cammiooi, Ma—. 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001646 

















































































REVISIONS 




SEE NOTE 3- 
2 PLACES . 



SEE NOTE 2 



notes: ^ 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. SURFACE TO BE FLAT WITHIN .015 TLR. 

3. BRAZE PER MIL-B-7883. . . 

4. FINISH—TIN PLATE PER MIL-T- 10727 TYPE H (HOT DIP). 

5. PAN HEAD SCREW, CRES, NO.4 -4QNC-2A *5/lfc LG PER MS35Z33-I4. 



CASE-MACHINED 
SCREW 


11001646 


NOMENCLATURE 
OR DESCRIPTION 


I | IDENTIFYING* NO. | ^TOWCATION 

LIST OF PARTS AND MATERIALS _ 


E>EE NOTE 5 

MATERIAL 
OR NOTES 


_ 100028 B 

_ 1000286 

NEXT ASSY USED ON 

APPLICATION 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANQLES 


DO NOT SCALE THIS DRAWING 
MATERIAL: 


M I T 

I NSTR UMENTATION LAS 
CONTRACT 


”2 

CHtCKEP 

PRAWN V. 

APPMVO FOR MSC 


CASE ASSEMBLY 


UNIT WT. I CODE IOENT. 


(lT/H. APPROVAL 

^ ll 


MIT 

INSTRUMENTATION 

LABORATORY 

_ CawR iPQK. Ma—. 

MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO. 

1001647 

























































3 



NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH STANDARDS PRE 

2. BREAK ALL ^HARP EDGES .010 MAX 


2 

























NOTES: 

1. INTERPRET DRAWING IN ACCORDANCE WITH MIL-D-70327. 

2. BREAK ALL SHARP EDGES .010 MAX 


REVISIONS 



























































jjb^l 

f.L 
% >' 






£ v '-| ; > 

1*. f 

, 0 ■'*•• 

■ * 

i T i 

*f : • :i 


: • « 

-,v 







tm mm 
















































































































Sir 

















































notes: 

1. UNLESS OTHERWISE INDICATED { 

ALL RESISTOR VALUES ARE IN OHMS 
ALL CAPACITOR VALUES ARE IN UF 

2. R4 8R5, RI4 8RI5 TO BE SELECTED AT TEST 
RANGE OF VALUES FROM I7.8K OHMS THRU 
30.IK OHMS 

3. RI3 TO BE SELECTED AT TEST 

RANGE OF VALUES FROM I.5K OHMS THRU 

2.4SiK ShVIS 

4. RI8 (EXTERNA! FEEDBACK RESISTOR) VALUE TO BE 
SELECTED AT TEST RANGE. OF VALUES FROM IK OHMS 
THRU 30-IK OHMS 


5. WINDING RESISTANCE FOR ACCEPTANCE TESTING 
CONTROL WINDINGS 154 I2%0HMS EACH 
TERMINALS 6 85, 3 84 BOTH CONTROL WINDINGS 
SHALL BE MATCHED WITHIN 0.1 OHMS. 

6. &7 ro be selected at test 

RANGE OF VALUES FROM 5K THRU t5K OHMS 

7. INTERPRET DRAWING /N ACCORDANCE WfTN 
standards prescribed by MIL • D - 70327 



© © 
I I 


TELEMETRY 

OUTPUT 


___ REVISIONS _ r, , ? 

I SYM DC SCRIPT ION ~ 1 DAT! | APPROVAL 

A REUSED PER TQRR 05353 Ta-o-fr l KX 
3 RE//SCD PER TDRR 06 06 3 
C &ZV/SED PER 7 QRR 3070 3 



REF 

DFS 

PART NO. 

DESCRIPTION 

VALUE 

TOL 

RATING 

Rl 

1010694-11 

RESISTOR 

" 63.4 

±1% 

I/IOW 

R2 

R3 

"i 

1010694-96 


487 



R4 

1010694- 


SEE N0TE2 



R5 

J0/C694 


Jl 



R6 

ICI0094--<)6 


487 



R7 

R8 

1010094- 
"}ofOC?4 - ’30 


NOTE 6 
UIK 



R9 

t0tO<bJ4--13O 


I.IK 



RIO 

JO 10095 -so 


187 


1/8 W 

Rl 1 

JClO(o95~9^ 


487 


I/8W 

RI2 

JOJO(b94-l2(j 


IK 


I/IOW 

RI3 

JO JOG 94 


SEE NOTE 3 



RI4 

JO 10694- 


SEE NOTE 2 



RI5 

/O/O694. 





RI6 

JOJOG95-96 


_487_ 


1/8 W 

Cl 

T0OG755-I0 

CAPACITOR 

4.7 

10% 

10 V 

02 

/0O675 5-/0 


4.7 

1 . 

10 V 

C3 

1006755-19 


3.3 

_L_ 

15V 

C4 

1006739-009 

f 

56 

7 

8V 

CRI 

" 1010497 

DIODE 

500 PI V 


3.4 W 

CR2 






CR3 






CR4 






CR5 






CR6 






CR7 






CR8 






CR9 






CRIO 



Y _ 



CRH 

7o/0216-2 


INJS8B 

5% 

4-00 M IV 

CRI2 

1010439*2 


5.8V 

5% 

2 50 MW 

LI 

100(550 

REACTOR 




L2 

100154-0 

: .i_..::. 




Tl 

100154-9 

TRANSFORMER 

— 

— 


R\8 

" IOIO3T1" 

‘resistor 

'see'NOTH 

t\% 

I/IOW 



DIMENSIONS AM IN INCHES 
TOLERANCES ON 

FRACTIONS DECIMALS ANGLES 


LIST OF PARTS AND MATERIALS 

SCHEMATIC 


_ tOOn? 84 

NEXT ASST USED ON 

APPLICATION 


00 NOT SCALE THIS DRAWING 
MATERIAL: 


INDICATING BRIDGE 
AMPLIFIER 


MANNED 

SPACECRAFT CENTER 
HOUSTON TEXAS 
NASA DRAWING NO 


IP 0 IPS 0 

<CT I 0. I 




3 


2 


1 


1001650 






























| REVISIONS C X ' , ; I 

ZONE 

SYM 

DESCRIPTION 

DATE 

APPROVAL 


A 

REVISED PER TORE 0535J 


~w~ 


3 

RE /IS CD PER TDRR 06 06 3 

/- 31-64- 

7/3 ^ 


C 

&EV/SED PER 72 MR 30709 

sE 

A- 

fePTu 


o 

eey/s£o /&e rme 2/5/j 



2113V RMS. 
3200 CPS 
SQUARE WAVE 


TELEMETRY 

OUTPUT 


REF 

DES 

PART NO. 

DESCRIPTION 

VA 

LUE 

4 

TOL 

~±(%~ 

RATING 

" I/IOW 

Rl 

1010694-11 

RESISTOR 

63 

R2 

i_ 



♦ 





R3 

10/0694-96 



487 





R4 

IOtOQ>94. 



SEE NOTE2 





R5 

1010 694 



i_. 





R6 

1010094 -96 



487 





R7 

R8 

10/0 

7o/o€ 

644 



notes 





>94-13? 



I.IK 





R9 

101069 4-/30 



I.IK 





RIO 

)o 10695-56 



187 



1/8 W 

Rll 

1010695-96 



487 



1/8 

w 

)W 

RI2 

1010694-126 



IK 



l/IC 

RI3 

10106 94 



SEE 

40TL 3 

MTE2 





RI4 

10106 9 4 



SEE 





RI5 

RI6 

/O/O 

IOIOC 

6 94 . 



r* 



W 


795-96 



487 



1/8 

w 


— 1 




Cl 

/OOG755-IO 

CAPACITOR 

4.7 

10% 

IOV 

C2 

/0Q6 

1006' 

755-10 



4.7 



10 

V _ 

V 

C3 

755-19 



3.3 



15 

C4 

1006789-00? 

Li ' 


56 



8V 

CRI 

1010497 

DIODE 

500 PI V 


3.4 W 

CR2 










CR3 










CR4 










CR5 










CR6 










CR7 

CR8 



















CR9 








— 

r — 

CRIO 

CRN 

CRI2" 

LI 








ioioe 
1010 

loot. 

330-2 



IN9E8B 

5% 

400MW 

439-£ 

550 

540 


- 


5.8V 

5% 

250MW 

RE AC 

tzj 

:tor 




L2 

1/00/ 






_ 











Tl 

1001549 

TRAN 

RES 

SFORMER 




RI8 

1010 311 

STOR 

SEE NOTE4 

♦ 1 % 

I/IOW 


notes: 

L UNLESS OTHERWISE INDICATED; 

ALL RESISTOR VALUES ARE IN OHMS 
ALL CAPACITOR VALUES ARE IN UF 

2. R4 8R5, RI4 8RI5 TO BE SELECTED AT TEST 
' RANGE OF VALUES FROM I7.8K OHMS THRU 

30.IK OHMS 

3. RI3 TO BE SELECTED AT TEST 

RANGE OF VALUES FPOM I.5K OHMS THRU 
2.49K OHMS 

4. RI8 (EXTERNAI FFEDBACK RESISTOR) VALUE TO BE 
SELECTED AT TEST RANGE OF VALUES FROM IK OHMS 
THRU 30-IK OHMS 


5. WINDING RESISTANCE FOR ACCEPTANCE TESTING 
CONTROL WINDINGS 154 12%0HMS EACH 
TERMINALS 6 85,384 BOTH CONTROL WINDINGS 
SHALL BE MATCHED WITHIN 0.1 OHMS. 

6. *7 to Be. selected at test — 

RANGE OF ML a£.3 FROM THRU tSKOHMS 

7. INTERPRET DRAWING IN ACCORDANCE W/rN 
STANDARDS PRESCRIBED BY MIL. - D • 70327 




UNLESS OTHERWISE SPECIFIED 



DIMENSIONS ARE IN INCHES 



FRACTIONS DECIMALS ANOLES 






DO NOT SCALE THIS ORA WING 


1000284 

MATERIAL: 

NEXT ASSY 

Used on 

| APPLICATION 



QTY I NOMENCLATURE 

REQO | OR DESCRIPTION 

PART OR 
IDENTIFYING NO 

1 

S 

MATERIAL 

OR NOTES 

FIND 

NO 

LIST OF PARTS AND MATERIALS | 


M I T 

INBTBUMFNTATION LAB 

CONTRACT 

nas rmr 


I f:,V b-2-Ti l 


*m«ovcd fom MSC 

r /(L APPROVAL I DATE 




SCHEMATIC 

INDICATING BRIDGE 
AMPLIFIER 


SCALE 

NONE 


1001650 


i <» i 


O 

in 

LO 

o 

o 
















































































































































L GENERAL 

MNTERPRET ORATING IN ACCORDANCE WITH MIL-D-TD527. 
^SUPPLIER SHALL CONFORM TO QOAUTt ASSURANCE 
PROVISIONS 5PECIPED IN ND10\S4e>4 CLASS). 

E INSPECTION AND ACCEPTANCE. 

. A-MECHANICAL REQUIREMENTS 
~ y DIMENSIONS 

3l detail specifications 

I) MIRROR TO BE PLAT TO V FRINGE OVER ALL VHTH 4 
FRINGE MAY IRREGULARITY. 

4. FINISH- ALL surfaces EXCEPT SURFACES marked 
~ AND HARDWARE TO BE FILLED AND RUBBED 

M SMOOTH (IF NECESSARY) AND PAINTED WITH 

A MINIMUM OF TWO (*) COATS OF ENAMEL 
' COLOR /FEO STD 5AS .CHIP NO. EGZSl 

5) 5LIDENTIFY PER NDlOOEOlD 

T 3 I± 005 - 


DRILL NO. 55 (.052} x .250 DEEP 
4 HOLES LOC AS SHOWN 


: —| - lOOO 

/ .500 


1.000±,020 R TYP 5 PLACES 


C> |)«M»D PW.I m •*** ||»M 

rc» W fMS ** 

O* PSmNTT _ 

«L O.tVT » 4 ** ^ A* •»* 

C3 lADOEP <TD 4%) DM 

Ft »MO NOtt ^ 

M 6)X**f*0* WM^TMUC CuWfftMt 

-rt» ms ft«t e » A>mt ____ 

REVISED PCX EC? lOfrfrS* 

TO A A // g JP PATE A.* 



- ~5C* SURFACE SEE NOTE S 



-So 


-.569 ±.005 


W5»t.0O5. 


X SURFACES 

SEE NOTE A 





AT>1 ± .003 TYP 


—.625 D\A TYP REE 

© 



•9.250 REE 


PROCURE ONLY FROM APPROVEO SOURCES LUSTED 
IN NO tOO20S4 FOR TH*S DRAWING 



FOR INFORMATION ONLY 

CLASS B RELEASE TDR No. DATE f/?/i <j 





MATERIAL I SPECIFICATION 


LIST OF PARTS AND MATERIALS 


UNLESS OT HERWISE SPECIFIED "^MAN INSTRUMENT CORTORATION 

DIMENSIONS ARE IN INCHES KIC 02"2>fi ^DOO l”55 


MANNED 

SPACECRAFT CENTER 

HOUSTON. TEXAS 


8.219 -i 
REF 


°"1- 0NAWN8jMiDy^0ATEuZijfa MIRROR, M)JUSTfcBLE IS 

DO NOT SCALE THIS DRAWING r M . c «^WAlbSEMBLY 

_ Jt SPECIFICATION CONTROL DRAMRN4 


A 43) REF 


NEXT ASSY I USED ON 

APPLICATION 




I CODE IDENT NO.I SIZE I NASA NUMSER 


SCALE NONE Ineiont 




























8 


7 


REQUfflEMEHW 

MNTEWPRET DRAWING IN ACCORDKNCt WITH Mll-O-TO'527. 
^ fi-SWPPUER 5HAU. CONFORM TO QUALITY ASSURANCE 
PRCV\S\ONS 5PEC\FED IN NDIO\S40^ CLASS!. 

Z. INACTION AND ACCEPTANCE. 

_A-MECHAN\CAL REQUIREMENTS 
-0 DIMENSIONS 

A DETAIL 5P^\F\CKT\ONV , i 

Z~ 0 MIRROR TO BE FLAT TO k FRINGE OVER ALL VIYTW $ 
rr_lFRINGE MAX IRREGULARITY. 


701 ±1005 



DRNJL NO. 55 (.052^ X .250 DEEP -=■ 
4 HOLES LOC AS SHOWN 


PROCURE ONLY FROM APPROVED SOURCES USTOO 
m NDfeMO** fOR WS PRAWiNa -~ r —■ 














































































REQUIREMENTS 

I.GENERAL 

A-iNTERPRET DRONING IH ACCORDANCE 
WITH Mlt-D ”70327 

B-SUPPLIER SHALL CONFORM ^0 QUALITY 
ASSURANCE PROVISIONS SPECIFIED IN 
HD 1015404 CLASS 3 
2. INSPECTION AND ACCEPTANCE 
A”MECHANICAL REQUIREMENTS 
I- DIMENSIONS 
B- SPECIAL REQUIREMENTS 
I- MATERIAL: 

LID A CASE ALUMINUM ALLOY 6061*0 (.090THK) 
PER QQ-A-327 TEMRER-0 
CLOSURE .MALE A FEMALE: ALUMINUM ALLOY 6043-T42 
PER QQ-A-874 TEMPER T4Z 
HINGE: ALUMINUM ALLOY 6061 -T6 

PERQQ-A” 270 TEMPER T6 
LATCH ASSY, BODY l STRIKE : STEEL 
HANDLE ASSEMBLY:- 
PLATE : ALUMINUM ALLOY 3003 "HU 

PER QQ-A-359 TEMPER HIE 
SPRING: STAINLESS STEEL 


BAIL •' STEEL AISI 1010 /-”x 
PER QQ-S-6^ O' 

GRIP: RUBBER 

PER MIL-R-6G5S,CLASSJl,6RADG 60. 
SEAL: NEOPRENE 

PER MIL-ft-665S,CLASS U, GRADE 6& 
FOOT-* ZAMAK NO. S 

PER QQ.-1-363 

LABEL: ALUMINUM FOIL PRESSURE 
SENSITIVE 

PRESSURE EQUALIZER ASSEMBLY 
•VALVE : ALUMINUM ALLOY tOZ 4 
PER QQ-A-26S 

• LOSE WASHER, NUT & RETAINING RING? 
STEEL 

0* RING, INNER £» OUTER 
RIVET: ALUMINUM ALLOY 
E-FINISH : 

LID * CASE; CLOSURE,MALE A FEMALE 
WASH PRIME PER MlL-C-1532* 

ZINC CHROMATE PRIME PER MIL-P-8S8S 
DU PONT NO. 93-91407 OR EQUIV. 

SYNTHETIC ENAMEL CASHMERE BLUE. 

LATCH ASSEMBLY CADMIUM PLATE 
PER QQ-P-416 

PRESSURE EQUALIZER ASSEMBLY ^ 
VALVE BLACK ANODIZE 

PER MIL-A”8 6tS,TYPE I. 
HANDLE A5 SEMBLY: 

PLATE : CAUS TIC DIP 4 ANODIZE (*) 

PER Mll”A”8 6 25,TYPEI. 
SPRING: PASSIVATE 

PER MIL STD-171 


BAIL: CADMIUM PLATE 

PER QQ-P-416 Cl ASS Z, TYPE 2. 
5-LABELING .-SILK SCREEN .75 AMD .SO HIGH WHITE 
CHARACTER 5.06 WIDE LINES PER 
ND IOOZOIB UNLESS OTHERWISE 
SPrciFIED^TOBE DESIGNATED BY PURCHASE 
ORDER) 

4*IDENTIFY USING NASA DWG MO. REVISION LETTER,* 
MANUFACTURER'S SYMBOL PER ND 100 2013 
5. THIS CASE ASSEMBLY CONFORMS TO MIL-T-44S 
EXCEPT PARA 3.51.2 4 *IS WATERTIGHT PER 
MIL- STD ”108 TABLE m. 


PROCURE ONLY FROM APPROVED SOURCES 
ON ND 1002034 FOR THIS DRAWING. 














































REQUIREMENTS 

..GENERAL 

A-INTERPRET ORATING IH ACCORDANCE 
WITH MIL-D -70327 

B- supplier shall conform to quality 
ASSURANCE PROVISIONS SPECIFIED IN 
ND 1015404 CLASS 3 
Q. INSPECTION AND ACCEPTANCE 
A- MECHANICAL REQUIREMENTS 
1-DIMENSIONS 
B- SPECIAL REQUIREMENTS 
|- MATERIAL*. ‘ 

* tUD IrCASE ALUMINUM ALLOY 6061-0 (.090THK) 
PER QQ-A-32T TEMPER-O 
CLOSURE .MALE A FEMALE: ALUMINUM ALLOY 6063-T4* 
PER QQ-A-274 TEMPER T4Z 
HINGE: ALUMINUM ALLOY 6061-T6 

PERQQ-A* %10 TEMPER T6 ^ 

LATCH ASSY, BODY 5 STRIKE : STEEL ' 

HANDLE ASSEMBLY' * 

PLATE: ALUMINUM ALLOY 3003 -HU 
PER QQ-A-359 TEMPER HIE 
SPRING: STMNLESS STEEL * 

BAIL: STEEL MSI 1010 

PER QQ-S-634 ^ 

GRIP: RUBBER 

PER MIL-R-6#5S,CLASSJtt,<SRAD6 60. 
SEAL*. NEOPRENE 

PER Ml L-R-6655, CL ASS X, GRADE 60 
FOOT.* IAMAK NO. 5 

PER QQ-Z-36S 

LABEL: ALUMINUM FOIL PRESSURE 
SENSITIVE 

•PRESSURE EQUALIZER ASSEMBLY 
-VALVE ? ALUMINUM ALLOY 1024- 
PERQQ-A-E6S 

• LOCK WASHER, NUT 6 RETAINING RUM? 
STEEL 

V RING,INNER*. OUTER 
RIVET: ALUMINUM ALLOY 
E-FINISH *' 

LID * CASE; CLOSURE,MALE A FEMALE. 

WASH PRIME PER MIL-C-I5326 
ZINC CHROMATE PRIME PER MIL-P-8S6S 
,DU PONT NO. 33-91407 OR EQUIV» 
i SYNTHETIC ENAMEL CASHMERE BUIK. 

LATCH ASSEMBLY : CADMIUM PLATE 
PER QQ-P-416 

PRESSURE EQUALIZER ASSEMBLY 
V VALVE BLACK ANODIZE 

PER MIL-A-6615,TYPE I. 

HANDLE ASSEMBLY: 

PLATE : CAUS TIC DIP A ANODIZE 

PER MIL-A-6»Z5,TYPE t. 
SPRING: PASSIVATE 

PER MIL STD-Ill 
BAIL? CADMIUM PLATE 

PER QQ-P-444 CLASS4 TYPES 
S. LABELING.-SILK SCREEN .IS AND. 30 HIGH WHITE 
CHARACTERS.06WIDE LINES PER 
ND IOOZOI3 UNLES5 OTHERWISE 
SPrcmED(TDBE DESIGNATED BY PURCHASE 
- * ORDER) 

4» IDENTIFY USING NASA DWG HO. REVISION LETTER A* 
MANUFACTURER'S SYMBOL PER ND 1002019 
S. THIS CASE ASSEMBLY CONFORMS TO Mtt.*T-94f 
EXCEPT PARA 3.51.2 4 A IS WATERTIGHT PER 
MIL-9TP-K>6 TABLE m. 


PROCURE ONLY FROM APPROVED SOURCES 
ON NO 1006034 FOR THIS DRAWING. 






















































































VS^10Q\ 


Requirements : 

4. GENERAL 

A. INTERPRET DN<S \N ACCORDANCE WTH MlL-D-lOSST 

B. SUPPLIER SMALL CONFORM TO QUALITY ASSURANCE 
PROVW»\ON* SPECIFIED IN ND10IS404 CLASS 3 

2. INSPECTION AND ACCEPTANCE. 

A. MECHANICAL 

L DIMENSIONS ARE FOR REFERENCE OHCf 

B. MATERIAL 

Plate. 1 . e>R.o*»iA 

ruKTEv- *Ju\jn*\k»vi*A •__ 

_3 . \D^n>t\^ FEI^ KD \oo^o\^ : 


REVISIONS 


SYM 


ZONE 


DESCRIPTION 


DATE 


APPROVAL 



3.150 R 


4.72-1 DIA 


5.s\2. dia 



CKrtTK*tN6 

FLNT*. 


FOR INFORMATION ONLY 

CLASS B RELEASE TOR No. Qk 00 C. 


•* 

: it) 

: s -I 


DATE 

1 


l-lt-Li 

L»Jui 


F»ROCORe ONLY FROM ^APPROVED SOURCES 
LISTED ON ND1002034 FOR THIS DRASWING 


I0H44.T 


1QQ447 


APPLICATION 


ITEM 

NO. 

QTY 

REQO 


GOVERNMENT/NASA 
NO. 

KOLLSMAN PART NO. 

CODE 

IDENT 

NOMENCLATURE OR 
DESCRIPTION 

MATERIAL 

SPECIFICATION 

UNIT 

WT 





LIST OF PARTS AND MATERIALS 1 


UNLESS OTHERWISE SPECIFIED 


DIMENSIONS ARE IN INCHES 


TOL| 

ON 


FRACTIONS 

DECIMALS 

ANGLES 


! 

! + 


DO NOT SCALE THIS DRAWING 


MATERIAL 

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CONTRACT 


NEW YORK 


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NASA APPR0VA1 


MIT APPROVA 


SPACECRAFT CENTER 

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1 ADAPTER, TRIPOD 

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5 
























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notes: 

i-lNTERFHAET DW^ IN ACCORDANCE WITH MIL-D-TOEBT 

1-%U^PUIA SHALL COK1PORM TO QUALITY /kVWRK^CA BPSC-lFlED .VI MD I0IB4O4 CLASSB 
V- LEVEL - 

a- objective apeturc -L3?a »n 

fc- LCNCrTH-IS 114 MAX 

C- C» RCULAR LEVEL SENSITIVITY_4 HIM /MM 

4- TECHNICAL REQUIREMENTS 

A- THE. FOCUSINQ K.KAOC* SHALL EE REMOVED AMD THE POCUBINO* ELEMENT LOCAED 
AT INFINITY FOCUS 

B-th« unit ehvll maintain A TRUE MOQlEONTAiL UME OP %»G,MTCUOE& WITH RESPECT 
TO LOCAL VERTICAL WITHIN E Z EEC. ARC. WHEN THE UNIT IB LEVEL WITHIN t EM I MUTES 
OR ARC. THIS ALIGNMENT ACCURACY EH ACC EftWAIWTAIWEO FOR AMINIMOM OP A 
E4 HOUR PERIOD AFTER RICAUERATIOU. THE CIRCULAR CEVEC SHALL Re AUQNED 
TO THE IMSTRUVSMTS OPTICAL- AVIS IN ORDER TO MEET THE AEOVE REQUIREMENTS 
C“ THE OMIT SMALL MAINTAIN ITE HORIZOMTAL UME OP SIQHT(LOS) WITHIN t E SECOND ARC 
WHIM THE UNIT IE OPP EET PROM CEVEC WITHIM ± IS MINUTES OP ARC. THIE ALIGNMENT 
ACCURACY EH RCC RE M AIHTAIMED POR A MIMIMUM PERIOD OP E4 HOURS AFTER R6CAUSRATOM 
O- THEUKUT EH ACC EE MOOlPlED TO PROVIOE A CAMP MOUBINCr FOR RETICLE ICUJMIMATIOM. 

THE EYEPIECE EHACC BE REMOVED AMO ACCESS SHALC RE PROVIDED TO THE RETICLE ADJUST! HQ 
SCREW WITH THE CAMP HOUBlMQ INSTALLED 

THE SPECIAL reticle SHOWM, EHACC RE ALIQNED TO THE ©ABREL AXIS SUCH * ' ^ 

THAT THE CENTER OP THE STAR ClRCCE LIES IM THE HORIZONTAL PLANE WHIN TESTED 
I Vi ACCORD AMCC. WITH PARAGRAPH B ABOVE 
R. T»4E CIRCULAR LEVEL MUST REMAIN CENTERED WHEN THE INSTRUMENT IS ROTATED 340* 

_ BY MEANS of THE TANCEKIT SCREW KNOBS. . . — 

B- ITEMS EOFPUBD BY VENDOR 

A- FITTED HARD WOOS CARRYING* CASE WITH TOOC COMPARTMENT AND RECATED TOOLS 
©- SPARE BULBS £5) 

C- IDENTIFICATION 

A* IDENTIFY IN ACCORDANCE WITH WD 10020 IS, NASA PART MO, REV LETTER AND MFRS SYR 
T- INSPECTION 4 ACCEPTANCE 
A- PERFORMANCE 

I- INSPECT THAT ACCURACY OP 4© ABOVE IE ACHIEVED WHEN TARGET BUBBLE ON UNIX IB 
ACCURATELY CENTERED. PERFORM ANCE. TESTING with INDUCED TILT OP ±E MINUTER 
OP ARC WILL BE PERFORMED ON A PERIODIC, S\MRJE LOT BASIS 


S-Q4LABB FILTER TORE TIFPEN FILTER NO. 5B OR EQUIVALENT (BOO© BBOO K) 
S-MINIMUM BULB LIFE TO BE EOHEB 



RETICLE. ADJUSTING, SCREW 


CIRCULAR. LEVEL. 


—TWO(2^ CONDUCTOR CAEL.E (M»L<*B4^ 

SlXW FEET LONQ-, C,*P0I^ CONDUCTOR 
TO e>R HOT CONDUCTOR TO M. WHVTR 


'LAMP SOCABT 



+.e>l 


%.©4b(R£F) 


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CENTRAL. BTAR 
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CIRCULAR WITHU4 I SEC 


FOR INFORMATION ONLY 

GLAM • MUAK TDK Nh_££^LL_ MU 


-PROCURE OULV FROM APPROVED ‘SOURCE-. 

LIVED IM WDIOMOS4FORTHIE OR.KVJIM& 


| LIST OF PARTS AND MATERIALS 

| UNLESS OTHERWISE SPECIFIED \ \ MANNED 


SPEC.IAL RETICLE CONFIGURATION 
(ANNULAR Ring, and central, star are 

:_TRAKfePAREAirr, BACKGROUND l"S _ 

-J_— opaqucV....___: 


1 DO HOT SCALE THIS DRAWINO IcmcKlP^ 


^ CbPECIFICATIOM CONTROL. £ 

" -rm-TXT CMC IMMT MO. | tut MAM MMMM 

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MIT MW«m W I CALI I / I ~ WIMT &IF... ItMWT 


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± 


9991001 


NOTES 

REQUIREMENTS: 

1- GEUERKL." 

*.WTERVRET DW6 PER MU--0-7OS7T 
B. SUPPLIER SRM-L CONFORM TO QUALITY 
ASSURANCE PROVISIONS SPECIFIED IR 
NO 1015404 CLASS S. 

2- INSPECTION AND ACCEPTANCE s* 

A-MECHANICAL REQUIREMENTS 

I-DIMENSIONS 

3-MATERIAL. AND FINISH *- 
A-FIBER-GLASS GEE PER MIL-P-I811T. 
B-FUNGUS-PROOF PERMIL-V-ITS. 
i ' 4-NUMERALS ARE WHITE 

5- IDENTIFT PER ND 1002019 WITH NASA PART 

HUMBER, REVISION LETTER AND MANUFACTURERS 
SYMBOL. 



■ 

.031—*Jl»— 


PROCURE ONLY FROM APPROVED SOURCES 
LISTED ON NO 1002034 FOR THIS OWS. 


DASH 

NO. 

A 

±.032 

B 

±.005 

NUMERALS 

PRINTED 

(NO.OP TERMINALS) 

1 

1.125 

1. 531 

1 

2 

1.637 

2.093 

1 AND 2 

3 

2.250 

2.656 

1 THRU 3 

4 

2.812 

3.218 

1 THRU 4 

5 

3.375 

3.781 

1 THRU 5 

6 

3.937 

4.343 

1 THRU 6 

7 

4.500 

4.906 

ITHRU 7 

8 

5.062 

5.46Q 

ITHRU 8 

9 

5.625 

6.031 

•THRU 9 

O 

6.187 

6.593 

ITHRU 10 

II 

6.750 

7.156 

ITHRU II 

12 

7.312 

7.718 

ITHRU 12 

13 

7.875 

8.281 

ITHRU 13 

14 

8.43 7 

8.843 

ITHRU 14 • 

15 

9.000 

9.406 

ITHRU 15 

16 

9.562 

9.968 

ITHRU 16 

17 

10.12$ 

10.531 

ITHRU 17 

18 

10.637, 

11.093 

ITHRU 18 

19 

11.250 

11.656 

ITHRU 19 

20 

11.812 

12.218 

1 THRU 20 

21 

12.375 

12.781 

1 THRU 21 

22 

12.937 

13.343 

1 THRU 22 

23 

13.500 

13.906 

1 THRU 23 

24 

14.062 

14.468 

1 THRU 24 

25 

14.625 

15.031 

1 THRU 2 5 

26 

15.187 

15.593 

1 THRU 26 


r FOR INFORMATION ONLY 


CLASS B RELEASE TDR ! 


DATE 

W</ 


n 




A 


— 

FRACTIONS 

DECIMALS 

TOL 

ON 

♦ 

!,o*o 


APPLICATION 


ITEM 

NO- 

TV 


NO. 


CODE 

IDENT 

NOMENCLATURE ON 
DESCRIPTION 

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m 1 


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LIST OF PARTS AND MATERIALS 1 ■ 


DIMENSIONS AWE IN INCHES 


DO NOT SCALE THIS DRAWING 


SEE NOTE 9 


t c 03 386900846 THRU 0873| 


V*V L t 


CHECKED. 

APPROVAI 






NAM APPROVAL. 


tesBp£&M- 

»«t 


MIT APPROVAL 


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PLATE, DESIGNATION 

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CODE IDENT NO. 


SCALE NONE 


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NASA NUMBER 


10016 66 


SStSal l ,MttT ~ 


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— INTF^PPET DRAWING IN ACCORDANCE WITH STANDARDS PRESCRIBED 
HZl BY MIL-0-70327. 

ZZ_SUPPLiER SHALL CONFORM TO QUALITY ASSURANCE PROVISIONS 

I-SPECIFIED IN NASA SPECIFICATION ND 1015404, CLASS 3. 

TZ__FUSE3OLDER 3HALL MEET ALL REQUIREMENTS-LISTED 0N.TM1S-^ 

-- DRAWINul .- - 

“ INSPECTION AHD ACCEPTANCE : (SAMPLE) 

“-..MECHANICAL REQUIREMENTS: . ' « * irv • 

MARKING; IDENTIFY USING NASA DWG NO., REV LTR AND 
'll MANUFACTURER'S SYMBOL PER N0 1002010 

ELECTRICAE1PEQ0IREMENTS'. PER TABLE 1 T-V - _- 


Z.991001 


REVISIONS 

DESCRIPTION 


DATE APPROVAL| 


"~mTESL_.. 

K>_TEMPERATURE LIMITS i TEMPERATURE LIMITS APPLY 
^ ~ TO FUSEHOLDER ONLY. FUSE DEGRADATION MUST BE 

_Z_CONSIDERED AS AN INDEPENDENT EFFECT. 


threads 

r-TKNOB _ I 

[ I #- RESISTOR 

1 r*m 


DESIGN REQUIREMENTS I - - 

1. CURRENT RATING t 20 AMPS MAXIMUM* -1 . 

IjOPERATUm^BLOwir FUSE WILL CAUSE KNOB TO LIGHT. 

1 MATERIAL AND FINISH ». ._-• ... 

" BODYslMOLDED PHENOLIC 

KNOB*- HIGH TEMPERATURE POLYSTYRENE, FREE OF CRACKS 
OR CRAZING!SMALL BUBBLES AND NORMAL WELD LINES 
;-ARE ACCEPTABLE. 

.._L1 CAP INSERTS BRASS, BRJGHT ALLOY PLATE. „ ^ 

—■— TERMINALS* BRASS, HOT SOLDER DIPPED (40% TO 70% 

" TIN CONTENT) ExdEPT INSIDE SURFACE OF END TERMINAL HOLE. 
"T" SPRING : STAINLESS STEEL 
ii:r nut*, steel* zinc plated and chromate dipped 

11_ FLAT WASHER: NEOPRENE 

HXDCKWASHER: PHOSPHOR BRONZE, NICKEL PLATED 
" CORROSION RESISTANCE; ALL METAL PARTS SHALL BE TREATED TD 
UJNITHSTAND QQ-M-151 SALT SPRAY TEST FOR 50 HOURS. 
ENVIRONMENTAL REQUIREMENTS: 

"_TEMPERATURE, ALTITUDE AND HUMIDITY * 

“ NON OPERATINGJ .- 

_TEMPERATURE? -37°C - 17I°C . 1,- . 

^IITZALTITUDE : 40,000 FT. 

—• — HUMIDITY : 95% FOR 12 HOURS 

* ‘l" OPERATING ■ -. 

- i&> ... TEMPERATURE l +IO®C - *0O°C 

_ ALTITUDE? O- 5000 FT. . 

- SHOCK? -22Y G'S, 11 MILLISECONDS 

HZH-.ViB.RAT LQMx lA — _ . 


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FIG. 1 


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KITH.FUSE INSTALLER _ 


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NUMBER 

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VOUAGE 

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RESISTOR 
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30 TO 300 

523E25BI5i 

4*1 

90 TO 300 

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INCANDE 5 CENTI 12 TO 33 


INCANDESCENT 13 TO 11 


NCANDESCENT 4 TO 6 


IMCAJ1DE5CENT C4 TO 13 


120,000 


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NOME 


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40 


COLOR 


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BLACK 


BLACK 




1/4 a | 1/4 

OCT 


1/4 A 1 1/4 

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RED 

1/4 A 1 1/4 

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RED 


~ PANEL CUTOUT (FOR REF) 
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BROINN 


BROWN 


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/FOR INFORMATION ONLY 

CLASS B KLEAAC TD* N. MIC *%£/ 


/(.<•«) drill 


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ION N0-1002034 FOR THIS DRAWING.. 


"o\w"- """To"/"*" io»T I "Te"^Ton°" | "* Tt ™ L | sstcincATiOM |“J 

-- LIST OF PARTS AND M ATERIALS 

iimi ccc nTUFDWKF SPECIFIED ROLLSMAN INSTRUMENT CORPORATIOW MANNED 

UNLESS OTHERWISE SPECIFIED - -■-<»■« . SPACECRAFT CENTER 

DIMENSIONS ARE IN INCHES KIC / g (5200 1401 THRU 1407 HOUSTON. TEXAS _ 

FRACTIONS DECIMALS ANOLES r " L-_ 

r°L I-T“^-- . TITLE 

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DO WOT scale this DdAwiwa chicaio P 4 t — (LIGHT INDICATING TYPE ) ' 

*‘ T “ ,Al Wjr 1 ' fini s - SPECIE ICAT10N-CONTROL DRAW ING 


MANNED 

SPACECRAFT CENTER 

HOUSTON. TEXAS 


J-MAEMPIT* 


DO NOT SCALE THIS DRAWING j cHECKEP. 

MATERIAL IAPPROVAL 


SATEfMii 

4-h-OA 


“SEE REQUIREMENTS. 


I CODE IDENT NO.I SIZE I NASA NUMBER 


XT ASSY | USED ON CONTRACT 

APPLICATION _ 


D 1001667 

[wEISHT SElW l ,H “ T I — " 







































































REQUIREMENTS: 


GENERALi 


IZ 9100 I 




REVISIONS 


DESCRIPTION 


DATE I APPROVAL 


ATINTERPRET. DRAWING IN ACCORDANCE WITH MIL-D-70327 
B.-SUPPUER3HALL CONFORM TO THE QUALITY ASSURANCE 
_ PROVISIONS SPECIFIED IN ND 1015404, CLASS 3- 
__:CL PRESERVATION, PACKAGING, AND SHIPPING. SHALL’BE IN 
ZL_ ACCORDANCE WITH MIL-P-3131, LEVEL A. 

“TAPE SHALL BE WOUND ON SPOOL OR ROLLS OF SO0 YARDS 
1 IN ACCORDANCE WITH; PARAGRAPH 3.10. 2 OF MIL-T*7I3 
“D. INDENTIFY USING NASA DRAINING NO., REVISION LETTER 
. -AND—MANUFACTURER'S-SYMBOL PER N D 100 TO 13. 

TTNSPECTtON AND“ACCEPTANCE: --~ r . ~ ~ 


A. TAPE WIDTH! SEE TABLE I - --_-__r_ 

3 .:tape'thickness s see table 11~.~r: . “::_;7i:.v;z, 

B. JIDRKMANSHIP SHALL BE IN CONFORMITY WITH PARAGRAPH 3.11 

:0F MiL-T-713 ' . : ‘ .. 

C. XOLOR;: natural - (WHITE) -— r :: 

ID BREAK ING SXRENGTH i SEE TABLE C, TESTED IN ACCORDANCE WITH METHOD 4102. 

TJEZFEDERAL SPECIFICATION CCC*T-l9l- _. - _ 

iSIGN ftEQTXIREM ENTS I ■ ., "I... • 

ZA. MATERIALT POLYESTER FIBERS, BRlOED, FLAT 

ZBI .FIN I5HI.Rt>BBER, SYNTHETIC, NON-FLAKING- 

C. FUNGUS~RE5ISTANCE SHALL BE IN ACCORDANCE WITH . ’ 

ZZZ PARAGRAPH 4. A, £_DF MlL=J-.U3 .EXCEPT THE TYPE OF 

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IDR AWING, - 


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J.7 - 40 .0361.003 ,029 -. 003 

' OH-— ' so; ... . .cnoxm .mist.,003 


FOR INFORMATION ONLY 


CLASS B RELEASE TDR Na£££^ 


DATE 


^SOURCES LISTED 


NEXT ASSY | USED ON 

APPLICATION 


rNote Y j-“ 00VERNM N0 NT/NA8A "OtLSMAN PART HO. ™ 


NOMENCLATURE OR 
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MATERIAL I SPECIFICATION 


LIST OF PARTS AND MATERIALS 


UNLESS OTHERWISE SPECIFIED KOLLSMAN INSTRUMENT CORPORATION 

^ ELMHURST NEW YORK 

DIMENSIONS ARE IN INCHES KIC /H AaCA1 1AO-7 

-rFRACTIOHsI DECIMALS I AHoT7T~ ™ 60Q3503 lUOl * iOOZ 


MANNED 

SPACECRAFT CENTER 

HOUSTON, TEXAS 


DO NOT SCALE THIS DRAWING IcHFotrp 


SEE REQUIREIAEMIJlA 


sssr "r,fE"S rrsPE^AcmcAHDTtms- 




CODE IDENT NO ■ SIZE | NASA NUMBER 


I NASA APPROVALS 


C 1001670 


ACTUAL 1 8HEET 1 0F 1 















6 


5 


2 


REQUIREMENTS: I— 

1. GENERAL: 

A. INTERPRET DWG IN ACCORDANCE 
WITH STANDARDS PRESCRIBED 
BY MIL-D-70327 
£>. SUPPLIER SHALL CONFORM TO 
QUALITY ASSURANCE PROVISIONS 
SPECIFIED IN NDI0I5404 CLASS 3 

2. INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS 

I. DIMENSIONS 
Z. MATERIAL 

CABLE-NYLON PER MIL-C-5424 

FERRULES-COPPER, ZINC PLATED (PjrRRULE to BE LEFT UNCRIMPEP ONE END) 

. b. IDENTIFICATION-IDENTIFY USING NASA 
PART NO., REV LETTER ( MFRS 5YM 
PER NDI0020IS ■ ■ 


zmoo\ 


SYM ZONE 


REVISIONS 

DESCRIPTION 


DATE APPROVAL 


B D1A 




C DIA 


DASH 


A+195 R+-0I5 
NO. P -.0I0 

-I 8.000 .156 


.063 


FOR INFORMATION ONLY 

CLASS B RELEASE TOR Ito. !/£ 7Z. DATE 


PROCURE ONLY FROM APPROVED SOURCE 
LISTED IN NDI002034 FOR THIS DWG 


APPLICATION 


jlTEM QTY 8YM GOVERNMENt/nASA I 


KOLLSMAN PART NO. 


NOMENCLATURE OR 
DiISCRIPTION 


SPECIFICATION 


LIST OF PARTS AND MATERIALS 


UNLESS OTHERWISE SPECIFIED KOLLSMAN INSTRUMENT CORPORATION 

I ELMHURST_ NEW YORK 


DIMENSIONS ARE IN INCHES 
I FRACTIONS | DECIMALS I ANGLES 


6020180100 


ttw l- ^ |!.OZO|!/V drawn K.GRU&LEfc »T, 5-a<-H 
DO NOT SCALE THIS DRAWING checked /ZtWrSte&Tt 


SEE NOTE 2. 


MANNED 

SPACECRAFT CENTER 

HOUSTON, TEXAS 


CABLE 

SPECIFICATION CONTROL DRAWING 


USED ON I CONTRACT 


I NASA APPROVAL. 


I MIT APPROVAL* 




CODE IDENT NO.I SIZE I NASA NUMBER 


1001672 


I SCALE NONE 


11 


























8 


10 


9 


REQUIREMENTS 


I. GENERAL: 

a) INTERPRET DWG N ACCORDANCE WITH MIL D*70327. 

b) SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE 
PROVISIONS SPECIFIED IN NDI0I5404, CLASS 3. 

e. INSPECTION i ACCEPTANCE: 

a) MECHANICAL REQUIREMENTS: 

I-DIMENSIONS AS SHOWN. 2-CERTIFIED CALIBRATION 
B. DETAIL SPECIFICATIONS- 

a) BASE-CAST IRON, THREE 2 IN. CASTERS 

WITH RUBBER TIRES (RETRACTABLE) 

5 ADJUSTING SCREWS WITH LOCK NUTS. 

b) MAIN TUBE. SEAMLESS STEEL TUBING WITH A 

BRONZE CLAMPING COLLAR BRAZED 
TO UPPER END, AIR CUSHION, BRACES 
C) INTERMEDIATE-HARD CHROME PLATED, RACK ATTACHED 
TUBE TO TUBE, INTERCHANGEABLE INSTRUMENT 

MOUNTS, OPENING OF ȣ IN. THRU CTR 
OF BASE AND INTERMEDIATE TUBE 
4) CONTROLS- - CAPSTAN, RACK PAWL AND CLAMPIN6 LEVER- 
CHROME PLATED. CAPSTAN SPOKES AND 
CLAMPING LEVER ARE TERMINATED IN 
BLACK PHENOLIC KNOBS. 

e) INSTRUMENT MOUNT. 1/2 IN. COORDINATE MOVEMENT 

3VWNS-2 THREAD. 

f) WEIGHT-STAND ONLY* 220 LBS APPROX 

SHIPPING -170 LBS APPROX 

4. FINISH: 

a) PREPARE ALL SURFACES PER ND1002098 

b) PAINT BASE EXTERIOR SURFACES USING 3 COATS 
OF FED- STD-595 COLOR NO. 26251 (DARKGRET) 





5. IDENTIFICATION: 

•) IDENTIFY USIN6 NASA PART NO., REV LETTER 
AND MFRS SYM PER NDI0020I9. 

4. SPOT DR NCX 55 (-052) . 167 DP AND ATTACH 

IDENTIFICATION PLATE NO. 1019345 USIN6 4 ROUNDHEAD 
DRIVE SCREWS NOs. MS21318-1 AT K.I.C. 



RACK 





PROCURE ONLY FROM APPROVED SOURCES 
LISTED m NDIOO£034 FOR THIS DRAWIN6. 


PIN 



PARTIAL 








FOOT PEDAL 

PRESS PEDAL TO RETRACT CASTERS - 
INTO THE BASE 

PRESS PEDAL TO LOWER CASTERS - 
OUTQPXHE BASE _ 


-SEE NOTE 6 
CENTRALLY LOCATE 
APPROXIMATELY AS SHOWN 


12 m. APPROX- 


- HEIGHT: 42|l H. CLOSED- 

24 IN. TOTAL TRAVEL 


FOR INFORMATION ONLY 

CLAW B RELEASE TDR Pte. MTE 


I LIST OF PARTS AND MATERIALS 

[ UNLESS OTHERWISE SPECIFIED *!*}-}*** «ST»UMEHT OOmMTIM | MANNED 

I DIMENSIONS ARE IN INCHES KIC ft 9 1 . 4 / rtl T o I SPACECRAFT CENTER 


! 02386900176 


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DO NOT SCALE THIS DRAWIH6 .... CTAI saicaw | 


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INSTRUMENT STAND 

( 5 PECfFrCA 770 N CONTROL DR 4 WJNS) 

CODE IOINT NO. SIZE NASA NUMIER 

F 1001673 


6 


5 














































9L 91001 


SYM ZONE 


REVISIONS 

DESCRIPTION 


DATE APPROVAL 


requirements 


I. GENERAL.* 

AikITERPRET DRAWING IN ACCORDANCE 

WITH STANDARDS PRESCRIBED BY MIL-D-70321. 
Br SUPPLIER SHALL CONFORM TO QUALITY 
ASSURANCE PROVISIONS SPECIFIED IN 
ND 1015404, CLASS 5 
2.INSPECTION * ACCEPTANCE 

a-mechanical REQUIREMENTS 
i. Dimensions 
3. MATERIAL*. 

STAINLESS STEEL AISU40C PER QQ-S-763 
CLASS 440C, CONDITION A*, HARDEN RC 55*58 
4 FINISH s PASSIVATE, PER MIL-STD-\1\ f 

(TABLE SA PARA 5.A. 2) 

5.IDENTIFY USING NASA PART NO. 

REVISION LETTER AND MANUPAC- l 

. TURERS SYMBOL PER HD 1002019. L —Z| 


. 250 D1A 


.1241 DIA 

♦.oooo 
_ -.ooo* 


I rota S'.-rcxI 
|!«M| 


FOR INFORMATION ONLY 


CLASS > RELEASE TOR Mo. DATE 

. ___ 


GOVERN ME NT/NASA I 


KOLLSMAN PAST NO. 


NOMENCLATURE OS 

DESCRIPTION 


MATERIAL I SPECIFICATION 


LIST OF PARTS AND MATERIALS 


UNLESS OTHERWISE SPECIFIED 


KOLLSMAN INSTRUMENT CORPORATION 

ELMHURST , NEW YORK 


DIMENSIONS ARE IN INCHES 


PROCURE ONLY FROM APPROVED SOURCES USTED 
ON ND 1002.054 FOR THIS DRAWING. 


I FRACTIONS I DECIMALS 


03386900910 


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REQUIREMENTS: 


|V 19^(001 


I. GENERAL: 

A. INTERPRET DWG PER MIL-D-70327. 

B. SUPPLIER SHALL CONFORM TO QUAUTT ASSURANCE 
PROVISIONS SPECIFIED IN NDI0I5404 CLASS 3 

2..INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS 
I. DIMENSIONS 

3. DETAIL SPECIFICATIONS 
A. SWIVFL CASTER-WITH LOCKING BRAKE - 

1. WHEEL MATERIAL: FORMICA * PHENOLIC MOLDED CANVAS 
WHEEL, MACERATFD CENTER, LAMINATED TREAD 

2. WHEEL SIZE: 4'DlA X I/i 
i TOP PLATE AND FORK MATERIAL: 

SMOOTH CASTINGS OF HIGH GRADE ALLOY IRON 

4. LOWER BALt PLATE: HEAT TREATED CASTING 

5. SAIL BEARING MATERIAL GRADE A CHROME NICKEL STEEL 
G. WEIGHT: a LBS EACH APPROX . 

b- RIGID CAGTTR- 

1. MATERIAL: SAME AS SWIVEL CASTER 

2. WHEEL SI ZE : 4" DlA X I ‘4 

3. WEIGHT: 4'/t LBS EACH APPROX. 

C. MOUNTING PADS' MATERIAL- STEEL 

D. DOLLY: MATERIAL-STEEL 

4. FINISH. 

A. PREPAREALL SURFACES PER ND 1002098 

B. PREPARE ALL SURFACES AiTH ZINC DUST PRIMER MIL-P-2G9I5. TYPE 1 
CLAS5 A,(E5-2C,4M) PER MIL-STD-508. CODE FIOI. APPLY 2 COATS.PER FED SPEC 7T-E-5Z3 
CLASS B,SEMI-GLOSS ENAMEL,COLOR 2C25I (DARK GREY) OF FEDSTD-535 PER NUL.-F-14072. 

5. IDENTIFICATION 

A IDENTIFY USING NASA PART NO., REV LETTER AND 
MFRS SYM PER ND 1002019 

6. SPOT DR NO. 55 (.052) .167 DP AND ATTACH 
IDENTIFICATION PLATE NO. I0I934G USING 4 
ROUND HEAD DRIVE SCREWS NO. MS2I 316-1 
AT K.I.C. 


0 


DESCRIPTION 

I REVVED PEE r.lP 


tp et//ftrr wer/*A* 


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SECTION A-A 


PROCURE ONLY FROM APPROVED SOURCES 
LISTED IN ND 1002 034 FOR THIS DRAWING 


FOR INFORMATION ONLY 


CLASS B RELEASE TDR Nfc.o££«£_ DATE 

‘AM 


10 


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101_9 


REQUIREMENTS: 


I. GENERAL: 

A. INTERPRET DWG PER MIL-D-70327. 
t> SUPPLIER SHALL CONFORM TO QUAtlTT ASSURANCE 
PROVISIONS SPECIFIED IN NDI0I5404 CLASS 5 
INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS 
I. DIMENSIONS 
S. DETAIL SPECIFICATIONS: 

A. SWIVEL CASTER - WITH LOCKING BRAKE 

I. WHEEL MATERIAL! FORMICA ’ PHENOLIC MOLDED CANVAS 
WHEEL, MACERATED CENTER, LAMINATED TREAD 
E. WHEEL SIZE: 4'DIAX I Vi 
§. TOP PLATE AND FORK MATERIAL: 

SMOOTH CASTINGS OF HIGH GRADE ALLOY IRON 
LOWER BALL PLATF: HEAT TREATED CASTING 
S. BALL BEARING MATERIAL’- GRADE A CHROME NICKEL STEEL 
G. WEIGHT: d LBS EACH APPROX. 

3 R161D CASTER - 

I. MATERIAL SAME AS SWIVEL CASTER 
1. WHEEL SI ZE ’ 4* DIA XI'4 

5. WEIGHT-’ 4‘/t LBS EACH APPPOX. - 

C. MOUNTING PADS•’ MATERIAL- STEEL 

D. DOLLY: MATE RIAL-STEEL 
4 FINISH: 

A. PREPARE AIL SURFACES PER ND1002098 

B. PAINT ALL EXTERIOR SURFACES USING 3 COATS OF 
FED-STD-595 COLOR NO. 26251 (DARK GRET) 

5. IDENTIFICATION: - „ 

A.IDENTIFY USING NASA PART NOl, REV LETTER AND 
MFRS SYM PER ND1002013 
G SPOT DR NO. 55 (.052) .187 DP AND ATTACH 
IDENTIFICATION PLATE NO. 101934G USING 4 
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4 


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section A-A 


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USTED IN ND 1008034 FOR THIS DRAWING 


3 


I 1 SZ0IOQI | 


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ISwmiAeT ...... 


LIST OF PARTS AND MATERIALS 


KOU$MAN IRSTRUMERT COtfOUATKHI 


j™ 02386900180 








MIT AAMOVAL. 




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REQUIREMENTS: 

1. GENERAL: 

A. INTERPRET DWG IN ACCORDANCE WITH 
STANDARDS PRESCRIBED BY MIL-D-70327 

B. SUPPLIER SHALL CONFORM TO QUALITY 
ASSURANCE PROVISIONS SPECIFIED IN 
ND 1015404 CLASS 3 

2. INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS: 

0 DIMENSIONS AS SHOWN 

2) MATERIAL: CARBON STEEL ,PER QQ-S-G33 

3) FINISH: CADMIUM PLATE PER QQ-P-416, 
TYPE I, CLASS 3 

4) THREADS'- PER MIL-S-7742 

B. IDENTIFICATION: 

IDENTIFY USING NASA PART NO., REV 
LETTER AND MFRS SYM PER NDI0020I9 


V 18 91001 


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DESCRIPTION 


DATE APPROVAL 


64 AbDEO ~ >» 

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I itemIqtyI government/n 

NO. pEQDl SYM NO. 


KOLLSMAN PART NO. 


NOMENCLATURE OR 
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PROCURE ONLY FROM APPROVED SOURCES 
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_|__ LIST OF PARTS AND MATERIALS 

UNLESS OTHERWISE SPECIFIED | KOLLSMAN INSTRUMENT CORPORATION I 


■ ELMHURST 

DIMENSIONS ARE IN INCHES K,c \ dCV 

IfRACTIONSI DECIMALS | ANGLES PN I 'Q\Jl 


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c 1001681 


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1 V^ 1 ' SCALE NONE WEIGHT 


1 



6 


3 


2 

















6 


5 


4 


REQUIREMENTS: 

1. GENERAL*. 

A. INTERPRET DWG IN ACCORDANCE WITH 
STANDARDS PRESCRIBED BY MIL-D-70327 

B. SUPPLIER SHALL CONFORM TO QUALITY 
ASSURANCE PROVISIONS SPECIFIED IN 
ND 1015404 CLASS 3 

2. INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS: 

0 DIMENSIONS AS SHOWN 

2) MATERIAL: CARBON STEEL ,PER QQ-S -633 

3) FINISH: CADMIUM PLATE PER QQ-P-416, 
TYPE I, CUSS 3 

4) THREADS’* PER MIL-S-7742 
B. IDENTIFICATION: 

IDENTIFY USIN 6 NASA PART NO., REV 
LETTER AND MFRS SYM PER NDI0020I9 



9 1891001 


- - REVISIONS,/^* 7 

L SYM ZONE_ DESCRIPTION _ DATE | APPROVAL 

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" SYM 
QD 

GOVERNMENT/NASA 

NO. 


CODE 

IDENT 

NOMENCLATURE OR 
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A. INTERPRET DWG IN ACCORDANCE WITH 
STANDARDS PRESCRIBED BY MIL-D-70327 
^ SUPPLIER SHALL CONFORM TO QUALITY 
ASSURANCE PROVISIONS SPECIFIED IN 
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18 91001 


1 REVISIONS 


SYM 

ZONE, 

DESCRIPTION 

DATE 

APPROVAL 









2. INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS: 

0 DIMENSIONS AS SHOWN 
! 2) MATERIAL: CARBON STEEL ,PER QQ-S-S33 

3) FINISH: CADMIUM PLATE PER QQ-P-416, 
TYPE I, CLASS 3 

4) THREADS'- PER MIL-S-7742 
B. IDENTIFICATION: 

IDENTIFY USING NASA PART NO., REV 
LETTER AND MFR5 SYM PER ND 1002019 




DA 6 H NO. 

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B±.OIO 

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DATE 


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ITEM 

NO. 

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B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE 
PROVISIONS SPECIFIED IN NDI0I540-4 CLASS 3 

2. INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS: 

1. DIMENSIONS 

2. MATERIAL - HAND KNOB* ALUMINUM 

^ SCREW t> SHOE-CARBON STL QQ-S-633 

3. FINISH* kOJoB-BLACK OXIDE PEC MIL-C-13*324 

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REQUIREMENTS'. 

1. GENERAL: 

A. INTERPRET DWG IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY MIL-D-70327 

B. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE 
PROVISIONS SPECIFIED IN NDI0I5404 CLASS 3 

2. INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS: 

1. DIMENSIONS 

2. MATERIAL-HAND KNOB'ALUMINUM 

SCREW $ SHOE-CARBON STL QQ-S-633 

3. FINISH-BLACK OXIDE PER MIL-C‘13924 

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8 


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REQUIREMENTS: 

1. GENERAL: 

A. INTERPRET DWG IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BT MIL-D-70327 
t>. SUPPLIER SHALL CONFORM TO QUALITY ASSURANCE 
PROVISIONS SPECIFIED IN NDIOI5404 CLASS 3 

2. INSPECTION AND ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS: 

1. DIMENSIONS 

2. MATERIAL* CfcflBON STEEL 4130, MIL-5*6758, HfclLT TREKT ROCKWELL C 35-40 

3. FINISH-BLACK OXIDE PER MIL-C-13324- 

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REQUIREMENTS ■ ... _ 

:; I.. general v z": .z: _ '~zz._ .; ' . z 

A) INTERPRET DRAWING IN ACCORDANCE 

WITH STDS PRESCRIBED IN MIL-D-70327. - 345 ~ 

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Z A) LOAD CARRYING CAPACITY TO 1000 LB TENSION. 

4. MATERIAL*. ' ~ - 

ZZ A) LATCH $ CATCH -STL: 5AE 4130 HEAT- TREATED 
Z B) ANCHOR PLATE- STL: ASTM A245 OR A4I5. 

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REQUIREMENTS: 

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1. GENERAL: 

A. INTERPRET DWG IN ACCORDANCE WITH 
STANDARDS PRESCRIBED BY MIL-D'70327 

B. SUPPLIER SHALL CONFORM TO QUALITY 
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2. INSPECTION £ ACCEPTANCE: 

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Ft'QlMPEMENTS: 

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A. INTERPRET P W IN ACCORDANCE WITH STANDARDS 
PRESCRIBED BY Mlt-D *70327 

B. SUPPLIER SHALL CONFORM TO QUALITY 
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C SPECIAL REQUIREMENTS- 

RUPTURE PRESSURE 7.5 PSIGt2. 5 PSIG 
CALIBRATE BY MAKING (2) RUPTURE DISCS 
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STAMP RUPTURE PRESSURE ON CALIBRATION 
TA6. 

2. INSPECTION £ ACCEPTANCE: 

A. MECHANICAL REQUIREMENTS 
. I. DIMENSION 
03. MATERIAL’. 

* A. FUNG - INNER AND OUTER - ALUMINUM ALLOT <SOC»l-T<* 

PER QQ-A-225/6 ,TEMPER TQ, 

6. SCREEN RETAINER- ALUMINUM ALLOT SOfet -TO, 

PER QO- A* 225/8, TEMPER "T& 

C. RUPTURE DISC - ALUMINUM ALLOT IIOO-HH 

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C. ALL SURFACES OF INNER AND OUTER RING AND SCREEN RETAINER TO SE 
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APPLY TWO (2> COATS OF CASHMERE SLUE ENAMEL PER NASA DWG NO. IOH.IS4 
TO SURFACES MARKED *T ONLY 

5. IDENTIFY USING NASA PART NO. RET LETTER AND MFRS SYM PER ND\0020tS 


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REQUIREMENTS : 

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A. INTERPRET DW<3 IN ACCORDANCE WITH STANDARDS 
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B. SUPPLIER SHALL CONFORM TO QUALITY 
ASSURANCE PROVISIONS SPECIFIED IN ND 
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G. SPECIAL REQUIREMENTS: 

RUPTURE PRESSURE 7.5 PSIGi 2.5 PSIG 
CALIBRATE BY MAKING (2) RUPTURE DISCS 
PER ASSEMBLY FROM SAME SHEET OF MATERIAL 
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STAMP RUPTURE PRESSURE ON CALIBRATION 
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2. INSPECTION £ ACCEPTANCE: 

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REQUIREMENTS 8 -7 - 

, I. GENERAL*. ' " - 

A-INTERPRET DWG IN ACCORDANCE WITH 
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B- SUPPLIER SHALL CONFORM TQ QUALITY 
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A-MECHANICAL REQUIREMENTS 7:7 :_ 7_7 _ 

: 1 -dimensions .' 

z- SPRING DATA 

A-MAX COMPRESSED LENGTH * 10.000 
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IDENTIFY USING NASA PART NO.) 
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f 


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QTY 

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SVM 

government/nasa 

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9"* *1 


NASA APPROVAL 1 


a. c*r„s)j u 


MIT APPROVAL 


& A&JpA/ofa/O* 


0 <Y^ MANNED 

SPACECRAFT CENTER 

HOUSTON, TEXAS 


POLYAMIDE(WYLONJ) PLASTIC 

: ADHESIVE BACKED 

SPECIFICATION! CONTROL DRAWING 


CODE IDENT NO. 


NASA NUMBER 


1001700 

jsHEET | OF I 


CALC 

ACTUAL 


c 


I 


f«on 


oo 


"■v 


INCHES 

‘L ««. <Ai i , J ,m, I d I 

O_ I g~ 

■ 'WWTUSRAPH»C «C*i Jf OWT | 















10 


9 


8 


6 



Rt ^OIREMENTS'. 


qe!'.eral-« 

A -Interpret OWC, PER. >A^D-7o3E7. 

SHALL CONFORM TO ®OAUTY PROGRAM 

_ QLIPEMENTS AS CONTAINED IN Mil-Q.-3858 
C.- S^PEC^L RE.GO VRAM'S HTS*. 

RETICLE DE^irh SHALL BE IN ACCORDANCE WITH 
PlUG loonoi S44T20F? 

t.*D€SIGN RE%OIREMEHTS 


- EFFECTIVE FOCAL. LENGTH - 

- FOCUS - - 


- magnification- 

-FIE’.D OF ViEvU - 


- 4B IKCHEB RJEF. 
-INFINITY 


•MWINUM WORVCIHQ DISTANCE- 

-ObJECTWC RESOLUTION- 

-SENSITWITT REPEATABILITY- 


- OC COLAR FOCUS RANGE - 

-scale Divisions - 


3.-INSPECTION AHO ACCEPTANCE .' 

-MECHANICAL REQUIREMENTS • 

~ OVERALL. DIMENSIONS 
-RCAomG Accuracy (full range) 

- «EAOMG ACCURACY (per OROWV rev) -i »/ 2 ARC- SECONDS 

-LIGHT SOURCE- VARIABLE \hTEHSiTY £ VOLT LAMP 

-Filter ..—.—. green- for *u«rou> baa»o (visual 

spectrum; light project** 

- OPTICS-AHTI- RE FLECTION COATED 

-POWER. INPUT- IIS VOLTS, CO CYCLES 

(JRAHSFORJMER ,RhEOSTAT AMO 
POWER CASlE. SUPPLIED. 


38 v 
26 ARC -MINUTES 
NSC FEET 
2.SACC-9EEDNO* 

*/io ARC- SECOND 
* BDiOPTERS 

SECONDS A HO TENTHS OF SECONDS, ONE MINUTE PER REVDlDTtQM 


-Barrel surface shall be straight 
VUITUVVI .000 25 OVER ENTIRE. LENGTH 
-FWED reticle TO BE CENTERED TO 
OUTSIDE. DIAMETER OF BAER&L WITHIN 
5 SECONDS OF ARC . 


DUST CAP 


-filter "to 8B. used with illuminating 
Source. Shall e>e scnott vss 

FILTER or EQUIVALENT 



* —COLLIMATOR TO BE SUPPLIED WITH 
HARDWOOD CARRvihG case with hinged 

COVER AND CARRYING! HANDLE 
NAMEPLATE. HO. 101937^ TO BE 
ADDED AT KIC USING FOUR (4) HO. 2 ROUND 
HEAD STAINLESS STEEL SCREWS PER MS 35495-201 
2> — AT Hie. APPLY PLATE IDENTIFICATION 
Ha IOIS 37 o BlHG* EC 81G 
PER WML-A-EOSZ. 

G>.-FINIS>W- fill IH cast SjORFACES and RUB TO 
A SMOOTH FINISH, IN ACCORDANCE WITH 
NO lOoeOBB. PARA. 3 C l . THEN APfV< 

5 COATS OF GRAY ENAMEL. .COLOR 
HO. EC 2SI OF FED-STD 


-18.750- 


12.875- 




-B.i49B±ggg$ DIA 



IDENTIFICATION 
SEE NOTE 4 


T 





5 


3 


2 


I 

I 



- EYEPIECE 
FOCUS ±190 




IDENTIFICATION PLATE. 
SEE NOTE £> 


I LIST OF PARTS AND MATERIALS _ 

UNLESS OTHERWISE SPECIFIED I "«S T * u **tN T C °*«)«ATI0II MANNED 

DiMtNsiows AM m imcmcs me ~SPACECRAFT CENTER 


00 NOT SCALE THIS DRAWING j 


2. INCH 

AUTO COLLIMATOR 

SPECIFIC At\0H CONTROL OWQ 

COOi lOtHT NO SIZE NASA NUMSC* 

E 1001102 



































202AOOV 


REVISION <ei*e »/.././I 

DESCRIPTION | DATE | APPROVAL | 


RETICLE , FIXED, BlFILAR 
$ matLtEleiaent no.imdTL-opt. class * 

Spec-RETICLE GlOKC 

TYPE.-C623- sac. 


REDSE TOL - 
OD- 


-L 52 5 
-B&.G 
clea* overlay 

CEMENT WITH LENS BONO M-62 
_ 12. MINUTES 
- BLAC* LAQuER 


m 


» LINES TO ®E BlACH ON CLEAR BY PHOTOGRAPHIC EMULSION 
PROCESS 

O ECX^E OF LINES TO be S'AOOTH aho clean unoelr. 

2F** MAC^N\rkCAT\ON 

COAT BOTH SIDES WITH ANTI-REEL JAM-T-VS (\<dO*T *A* TtPP.) 


*H t—.05 
- 00 

Hll—.oi' 


U—.050 TYP 


IK 


0 .000640 DIMS AS SHOWN IN DETAILAJO BE. EQUAL 
WITHIN .000040 


CURSOR , HORIIONTAL 

A) TOLERANCE ON ALL LINES t ioX OF stated VALUES 
NONv CUMULATIVE ON A G»IVElsl CURSOR, t S 7. 
TOLERANCE ALSO PERMITTED RANDOM DIRECTION. 

6) NUMERAL LINE THICKNESS TO BE .0018- 
C) LINES TO BE PHOTO REPRODUCED BLACK ON 
CLEAR. . OOOI MAX THICKNESS. 


.0590 - 

±.0038 


3l CURSOR , VERTICAL 

A') SAME NOTES AS NOTE 2. 


.098)4 ±0200 



.0123 TTP 
.0575 TYP 


-.0115 HIGH 


.0012 YllOE. FILAR LINES- 
( DEFECT .000E t*AYl) 



-.0100 BEY R. 


.0004 WIDE GRADUATION UNES- 
(DEFECT .OOOI VAAYL.) 



3337tS§§§ 

DIA. 


CURSOR, VERTICAL 

SCALE IO-.I 


I 


.0125 HIGH 


EMULSION sioe 


.0054 TYP ♦jfP f 
.OOZ7TVP—LW/ 


.0012 WIDE FILAR LINES 
(DETECT .0002 MAX.) 


n jyp-Vuj 

...riV 
.I 


.0006 WIDE GiRADUATlON LINES 
(DEFECT .OOOI MAX.) 


-.050 TVP 


RET\CA-E., F\*ED 

e>\F\LKR. 


\~r^. 

i 413 2 I 0 


__ «_ 

037 
.0125 TV 


L .0125 T VP 
.0094 TYP 


—H — .0125 TVP 


—.0250 TVP 


90 O* t O’ 2* 


CURSOR, HORIZONTAL 

SCALE IO : I 


.000900 *.000040- 
TYP 


.00875Ot .000500 TYP 


-.000350 t . 000040 


-SEE NOTE IE 


SEE NOTE 10 


.00064 0 —*|4- 

-*»j |p- .001280 t.000060 

CLEAR INSIDE 


DETAIL -A 
SCALE 100-1 


LIST OF PARTS AND MATERIALS 


UNLESS OTHERWISE SPECIFIED MiUMHUI IRSTAUMEWT CORMRATjOR 

—" Q\ 3&49000 SO 


DO NOT SCALE THIS DRAWING | C hh 


SEE NOTE » 


z men 

AOTOCOLUV\^OR. 

SPEC\T\CKT\ON CONTRO- DV<Gi. 




E 1001X2 











































S3 BIX 
S1 RED 



P3 BLK 
P2YEL 
PI RED 


64 &Z 


BLU YEL 


SCHEMATIC (FACING SHAFT) 


4 


3 


2 


1 












K*E 


6 


5 


REQUIREMENTS'- 

1. GENERAL'. 

A. INTERPRET DRAWING IN ACCORDANCE WITH 
STANDARDS PRESCRIBED IN MIL-D-70327. 

B. SUPPLIERS SHALL CONFORM TO THE QUALITY PROGRAM 
REQUIREMENTS CONTAINED IN MIL-Q-9858. 

C. UNITS SHALL BE CAPABLE OF MEETING ALL ELECTRICAL 
AND MECHANICAL REQUIREMENTS OF ND PS1QIOMI AND 
ND1002013 EXCEPT AS NOTED IN THIS DRAWING. 

2. ACCEPTANCE AND INSPECTION: 

A. MECHANICAL PROPERTIES: 

(I) MARKING: PER MIL-STD-ISO. PARTS SHALL BE 
PERMANENTLY AND LEGIBLY MARKED WITH 
THE MFR’S NAME OR SYMBOL, TYPE OR PART 
NO. £ SERIAL Na NAME PLATE TO READ FROM 
LEAD END. 


{Z) LEADS SHALL E»E TYPE E-26 PER MIL-W-IG876 
CONSISTING OF 7 STRANDS OF N0.3G AWG WIRE, 
INSULATED WITH EXTRUDED TEFLON. LEADS SHALL BE 
COLOR CODED. 

(S) RUNOUT OF DIA “A" SHALL NOT EXCEED .0005 HR WHEN 
MEASURED WITH THE UNIT IN A VERTICAL POSITION 
SUPPORTED BY THE OUTPUT SHAFT. 

(4) RUNOUT OF DIA *B“ SHALL NOT EXCEED .OOOBT.I.R. 

WHEN MEASURED WITH THE UNIT IN A VERTICAL POSITION 
SUPPORTED BY THE RESOLVER CASE. 

(5) SHAFT END PLAY NOT TO EXCEED .002 UNDER & 0l±\0l. 
MEASURING GAU6E LOAD. 

(4) RADIAL PLAY OF SHAFT MEASURED AT POINT NOT MORE 
THAN .125 FROM FRONT FACE OF CASE SHALL NOT 
EXCEED .0007 T.I.R. UNDER BOZ.±I/LOI. REVERSING 
GAGE LOAD APPLIED NOT MORE THAN .25 INCHES 
FROM FRONT FACE OF CASE. 

FRICTION TORQUE: 15 GRAM-CM MAXIMUM AT 25®±5*C 
ELECTRICAL PROPERTIES •' 

PHASE EQUATIONS: 

E^i-si * K Ep|-P2> COS0 - KEps-p3 SIN0 
Es 2-54- = K Ep£-p3 COS 0 + KEpi-pj SIN0 
9 IS THE SHAFT ANGLE DEFINED POSITIVE FOR 
COUNTER-CLOCKWISE ROTATION FACING THE SHAFT. - 

3. DESIGN: I 

OPERATING TEMPERATURE RANGE: -55°C TO ■H25 0 C. _ 
FRICTION TORQUE: 15 GRAM-CM MAXIMUM AT25*±5°C. _ 
CASE AND SHAFT MATERIAL SHALL BE CRES PER QQ-S-743 - 
LUBRICATION: BEARINGS SHALL BE LUBRICATED WITH " 
LUBRICANT SPECIFIED IN ND 1002077,6£. F-50 SILICONE I 


AD-1340 


6 


5 


4 


3 


2 









5 


3 


2 


SYM ZONE 


REVISIONS I'rjfg , j »/>*/({ 
DESCRIPTION I dATE I APPROVAL 


WOT£V. 

I - eE.QUlR£MEKlTS: 

A' lKlT£R.PRtXP\M6» IU ACCORPAKiCE 

WITH BTDe? PKE5CE(BEP BY MlL-P-70327. 

B- Supplies bhalucoufogmtotwb 
QUALITY PI20C.Sam RE.QUIK.eM€k)T3 

COUTAIUEP HU MlL-GJ-^&^S 
1- IKlSPEdTiOKi AUD ACCEPTANCE: 

A-MECHANICAL CEQUVeeMENTB 
(l) DIMENSION'S PEe OUTLIVE 
CO LEAP DATA ; LEAPS BHALL 6>S S0LI>eeA8LE 
(3) MARKlklC?'- PER MlL-STp-\30 PARTS 
SHALL BE LESIBL\ / <S-PERMAK)EKJTLY 
MAI2K.EP VJITU the manufacturers 
KJAME OP SYMBOL TYPE UO, y 
RESISTANCE VALUE CTOLEEAkjCE. 

B-ELECTRICAL eEC^O^EMElOTS: I— 

(l) RESISTANCE VALUES: PER TABULATION 

(24 RESISTANCE TOLERANCES ± \% 

(3)fower. Patino: J^watt 
3-desicn eccpuipEiuieiNTs i 

(I) UNITS SHALL MEET THE APPLICABLE j= 

REQUIRE ME NTS OP MIL-R- IO&OS [_ .026 

*3TYl_E RU GO OHARACTERISTICS .014 

CAUDE VUITH THE EXCEPTIONS 
3P&CIFIEP HEREIN). 


A S6 ^evisep PeRECPi09A3<b fc3o]65 AC,^ 
TDRR NO. 10237 ShSlfoS A-iP 


LC25 
1.37 5 


1.62$ 

1-375 



.024 


ITEM QTY GOVERNMENT/NASA 

NO. REQD NO. 


KOLLSMAN PART NO. 


NOMENCLATURE OR 
DESCRIPTION 


MATERIAL I SPECIFICATION 


J_—__ LIST OF PARTS AND MATERIALS 

UNLESS OTHERWISE SPECIFIED I KOLLSMAN INSTRUMENT CORPORATION I 

—-----I ELMHURST _NEW YORK I 


DIMENSIONS ARE IN INCHES 
T FRACTIONS | DECIMALS | ANGLES 


™ 03?>3<o'i>00'Z>+S 


MANNED 

SPACECRAFT CENTER 

HOUSTON, TEXAS 


ON + <\_j + "V- + -Y_ _ TIT “ 

' bL,sci;. thisJ;..,, - Rector, fixed, film 

,ATERIAL APPROVAL ii4 W _ l-'V-t* l/£>W 


SEE DOTES 


NEXT ASSY USED ON CONTRACT 

APPLICATION 


approval JU ^ I - f T * <» . V — ^ 

APP.OVA. & w,? Mtr specification cohtirol prawiu^ 

flm .\ A ‘ CODE IDENT NO.I SIZE NASA NUMBER 

NASAAPPROVAtiLlmj^A’- 


I NASA APPROVAL _ 


IMIT APPROVAL 


fj mc t,: 


• SCALE MOKlC 


ioo nos 

i sheet * 


5 


3 


1 


CLI OO 









IOOI 











































































































































































































































VOO. 

RESISTANCE 

| PASH WO. 

RESISTANCE 


jm 

OHMS 

KB 


: OMMS . 

Z65 

Z. £6? 

1180 

331 

332 

2610 

26.1 

u>a 

1210 

333 

334 

2670 

IK— 

210 

1240 

335 

336 

2740 

211 

272 

ISBS 

337 

338 

2800 

215 

274 

1300 

339 

340 

2870 

215 

216 

1330 

341 

r 342 

2940 

277 

278 

1310 

343 

344 

3010 

279 

280 

1400 

345 

346 

3090 

28l 

282 

1430 

347 

348 

3160 

285 

284 

1470 

349 

390 

3240 

Z85 

286 

1500 

351 

352 

3320 

287 

zee 

1540 

353 

354 

3400 

289 

29 0 

1380 

355 

356 

3480 

291 

29Z 

1620 

357 

358 

3570 

293 

294 

1650 

359 

360 

3650 

295 

296 

' 1690 

361 

362 

3140 

297 

298 

1740 

363 

364 

3830 

299 

300 

1180 

365 

36>6 

3920 

301 

302 

1820 

367 

36 a 

4020 

303 

304 

1810 

369 

370 

41 2o 

505 

306 

1510 

371 

372 

4220 

307 

308 

I960 

313 

374 

4320 

309 

310 

2000 

315 

376 

4420 

3|| 

312 

2050 

311 

378 

4530 

Si 3 

ELII 

2100 

319 

380 

4640 

ESI 

316 

2150 

SSI 

382 

47 50 

911 

318 

2210 

383 

384 

4870 

519 

320 

2260 

r 385 

386 

4990 

321 

322 

2320 

387 

388 

5110 

323 

324 

2310 

389 

390 

5230 

3 25 

326 

2430 

391 

392 

5360 

327 

328 

2490 

393 

394 

5490 

3Z9 . 

330 

2550 

395 _ 

396 

5620 


the complete pa zr wo. is the puj6 ioo. 

PLUS THE APPLICABLE OASH 100. 


AD-1340 


6 


5 




DASM WO 


7 dash WO 

kesistawce 


saa 

iHqq 

CHARAC 

C. 

.teristic 

1 & 

OHMS 

397 

398 

5760 

46 3 


12,700 

399 

400 

5900 

465 

1WR 

iimo 

401 

402 

6040 

461 


I1PLT»V 

403 

4-04- 

6190 

469 


■EfEEH 

405 

406 

G340 

47 1 

09 


407 

4-os 


473 


IESS3I 

409 

410 

6650 

475 


lOQOi 

411 

412 

6810 

477 

liffa 


413 

414 

6980 

479 

480 

o 

o 

4 

u\ 

415 

416 

7150 

481 

IBM 

■—7— 

411 

418 

1320 

483 

IBM 

f 16.200 1 

419 

420 

1500 

485 



421 

422 

7680 

481 


r 16,900 

423 

424 

7870 

489 


■mi — 

425 

426 

8060 

491 


17, 800 

427 

428 

8250 

493 


18,200 

429 

430 

8450 

495 


18,100 ' 

431 

432 

8660 

491 

P 4-98 

19, 100 

433 

434 

8870 

499 

500 

19, 600 

435 

436 

90-90 

501 

502 

20.000 

437 

43S 

9310 

503 

504 


439 

440 

4530 

505 

5 06 

Bln^^Wl^KK 

441 

442 

9760 

507 

508 

21, 800 

443 

444 

IQOOO 

509 

510 

mi 

445 

446 

10,200 

511 

512 

■§**7—1 

447 

448 

10, 500 

513 

514 

23, 200 

[449 

450 

10,700 

ESI 

516 

23.100 

451 

452 

11, OOO 

517 

Ban 

Eft£333HI 

453 

454 

11,300 

519 

520 

—CSS—1 

455 


11, 500 

521 

522 

1—SI 

457 

45a 

11,800 

523 

524 

26, IOO 

459 

460 

12,100 

525 

526 

26,700 

461 

462 

12,400 

521 

528 

27,4 OO 


1 


| SYM 

ZONE 

DESCRIPTION 

AVKJPI 

Esa 

r— ■v / v M -1 

APPROVAL 1 

U 


TO SHEET 1 

— 






— 


B 


NEXT ASSY 


USED ON 


applic ation 

4 


ITEM 

NO. 

QTY 

REQD 


go» ER nm E nt/na»* kolisman part mo COD E I 

NO - IDENT 1 

NOMENCLATURE OR 
DESCRIPTION 

MATERIAL 

SPECIFICATION U * ,T 
WT 



— 

LIST OF PARTS 

AND MATERIALS 




UNLESS OTHERWISE SPECIFIE D 

DIMENSIONS ARE IN INCHES 


FRACTIONS 


DO NOT SCALE THIS DRAWING 


MATERIAL 


CONTRACT 


ELMHURST 


033 8 680 054S 


DRAWN. Tlo m l i ir^ urr a- g- vt \ 


CHECKED | -1 - 6 S 


APPROVAL Jl 
APPROVAL. 






P 

NASA APPROVAL A 




MIT APPROVAL 


MANNED 
SPACECRAFT CENTER 

HOUSTON. TEXAS 


TITLE 


RESIST 0Z S FIXED FILM 


5PE0lPICATl0k) COUTgOL DgAuJlL)6> 


CODE IOENT NO.I SIZE 


NASA NUMBER 


iooiios 


SCALE UOkJt [WEIGHT 


CALC 

ACTUAL 


SHEET 


OF ^ 


3 


1 













































































































































































































6 


5 


DASH kiO. 


28,700 


939 

536 

30, IOO 

537 

538 


639 

540 


541 

542 

32,400 

B9 

544 

3 3, 200 

545 

546 

34, OOO 

547 

548 

34,800 

549 

550 

35,700 

551 

552 

36, 500 

553 

554 

37,400 

555 

556 

38,300 

557 

5>5B 

39, 200 

55? 

56 O 

40,200 

561 

562 

QESSEBI 

563 

£64 

42, 200 

565 

566 

43, 200 

567 


44, 200 

569 

570 

45, 300 

571 

572 

46, 400 

573 

574 

Ul, 500 

575 

576 

EUESSH 

577 

r 578 


579 

580 

51, too 

581 

582 

52, 300 

585 

584 

53, 600 

585 

586 

54,900 

5 87 

588 

56,100 

589 

590 

57, 600 

59 1 

592 

59, OOO 


6Q 4QQ 


DASH DO 

CHA(?AC 

c 

T ERISTIC 

£ 

595 

596 

597 

598 

599 

6©C> 

£>OI 

602 

603 

604 

605 

606 

607 

coa 

609 

CIO 

EH 

612 

<613 

614 

Ha 

IHQI 

HEH 

618 

BH 

620 

621 

622 

623 

•624 

625 

626 

627 

6 28 

629 

6 30 

EQQH 

632 

635 

^6 34 

6 35 

6 36 

6 37 

638 

639 

640 

641 

642 

643 

644 

645 

646 

647 

648 

649 

6 50 

651 

6 52 

Ce>£3 

6 54 

655 

656 

657 

658 


61,900 


65, lOO 


73.2.00 


1(0,300 


SO, 600 


88, 700 


9 3, IOO 


95, 300 


97, 600 


IOC> OOO 


102,000 


105, OOO 


107, OOO 


121,000 


127, OOO 


133,000 


Twe complete part do. isths pvuo ioa 
plus the applicable t>ash ho. 


AD-1340 



Ieoh smi 


REVISIONS f^a nr}J J/'i/t 


DESCRIPTION 

DATE 

APPROVAL 

REFER TO SHEET l 

- r- 


DASH MO. 



(fib>4r 

ligsjr-r.q 

665 

CpCp(p 

143,000 

667 

(p(pQ> 

147, OOO 


670 

I1ESE551 

671 

672 

154,000 1 

673 

674 


675 

676 

162,000 

677 

070 

165,000 

67 9 

680 

169,000 

681 

602 


6 83 

604 

IHEE23 

685 

6 86 

182,000 

667 

£ 

107,000 

689 


191,000 

691 

692 


693 

694 

I^EEI 

693 



697 

6 90 

210, OOO 

699 

700 

215,000 

lo\ 

702 

IES9EE3I 

703 

704 

226,000 

705 

706 

232,000 

707 

708 

237,000 

709 

710 

243,000 

711 

na 

249, OOO 

H3 

714 

255, OOO 

715 

«Mi 

261,000 

717 

na 

267,000 

n 

720 

274,000 

721 

722 

280,000 


287,000 


294,000 


DASH kJO. 


CHARACTERISTIC 
C_|_£_ 

727 

728 

729 

730 

7 31 

732 

7 33 

734 

735 

736 

137 

13B 

739 

740 

r74l 

742 

743 

744 

745 

746 

747 

748 

749 

750 

751 

752 

753 

754 

755 

756 

7 57 

758 

759 

760 

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762 

763 

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765 

766 


RESISTANCE 

OHMS 


301,000 


309.000 


316,000 


324,000 


332,000 


340. OOO 


34^000 


35-7,000 


374,000 


333,000 


392,000 


4-02,000 


412,000 


432,000 


493,000 


464,000 


475,000 


499,000 



g° v e r nment/nasa kollsman part mo code nomenclature or 

_NO*_IDENT DESCRIPTION 


_ LIST OF PARTS AND MATERIALS 


MATERIAL I SPECIFICATION 


UNLESS OTHERWISE SPECIFIED I KOLLSMAN INSTRUMENT CORPORATION 

-—_ | ELMHURST HEW YORK 

DIMENSIONS ARE IN INCHES | K 1C __^ 

pn 0^33630034^ 


Mif.mH.'HEBCngi 


DO NOT SCALE THIS DRAWING 


MATERIAL 


MANNED 

SPACECRAFT CENTER 

HOUSTON. TEXAS 


, nwS . RESISTOR FIXEP, FILM 

i/sv\J 

SP£CIFICATIOO CODTPOLX«?AVjJ»L16 


CODE IDENT NO.I SIZE | NASA NUMBER 


NEXT ASSY I USED ON CONTRACT 

APPLICATION 


oonos 


SCALE |OOUE I WEIGHT 


oonos 










































































































































































































































































































































5 


3 


2 


SYM ZONE 


REVISIONS 

DESCRIPTION 


,rs*? tfitr/es 
DATE I APPROVAL 


MOTES’. 

I - e.EQOlRe.MEMTS: 

A- »NT£epRETWJ6> IW ACCORDANCE 
WITH STDS PRESCRIBED By MlL-D-70327. 

B- SUPPLIER SHALCC/JUFOCliATOTHE 

QUALITY PR06-RAM REQUIREMENTS 
CONTAINED IVJ MlL-Q-^S^B 
L- INSPECTION AND ACCEPTANCE: 
a-mechakucal requirements 

(U DIMENSIONS P£e OUTLINE 
t) LEAP DATA *. LEAPS BWALL 6>E SOLPEEASLE 
C3) MAeKlMG*’. PEE MtL-STD-130 PARTS 
SHALL e>E L&£,IBlY£-PERMANENTLY 
MARKED VJITU THE MANUFACTURERS 
. klAME Op SYMBOL TYPE ND, ; 

RESISTANCE VALUE eTOLEEAMCE. 

P- ELECretCAL REQOH^&MEKyrS: h 

6 ) RESISTAMLE values: per TABULATION 
■ { 2.}PESISTANCB TOLEPAWGES ±\% r ,. 

1: POWER EATlNSl ATT 

3-DESIGN e&QLMRBKAENTS | 

(1 ) UNITS SHALL MEET THE APPLICABLE t-*= 

; REQUIREMENTS OF MIL-R-I030 4 ) T .026 

•STYLE PN 0,0 CHARACTERISTICS JD24 

CAUD6 VUlTHTHE EXCEPTIONS 
-SPECIFIED HEREIN). 

(^QUALIFICATION TESTING IS NOT 
REQOieEp EXCEPT TO NDlOO205>7 


\.G15 
LSI 5 


L375 



I qovernment/nasa 


KOLLSMAN PART NO. 


NOMENCLATURE OR 
DESCRIPTION 


SPECIFICATION 


LIST OF PARTS AND MATERIALS 


UNLESS OTHERWISE SPECIFIED 

DIMENSIONS ARE IN INCHES 
I FRACTIONS I DECIMALS I ANGLES**" 


KOLLSMAN INSTRUMENT CORPORATION 

ELMHURST NEW YORK 

pn C 0338fe?>00^>4S 


MANNED 

SPACECRAFT CENTER 

HOUSTON, TEXAS 


DO NOT SCALE THIS DRAWING Icheckep i 


SEE NOTES 


l-T(.S 

i-if-Lr 


/. RESISTOR,PIXED, FILM _ 

~nrz ~\/e>w 

iPEClFICATiOKi COKlT^OL PRAWIU6 p 


CODE IDENT NO.! SIZE I NASA NUMRER 


I NASA APPROVAL M 


loonos 


APPLICATION 































PASH WO. 

RESISTANCE 

PA3H mo. : 


PA5>H 



OHMS 

charac 

c 

TteiSTK 

e 

: OHMS.... 

CHARAC.T 

C 

■m 


49.9 

! 67 

60 

no 

133 

3 

4 

51.1 

(&9 

70 

113 

135 

5 


52.3 

■hi 

72 

115 

137 

7 

s 

53.6 

73 

74 

118 

139 

.9 - 

IO 

549 !. 

75 

76 

121 

141 

ii:. 

12 

56.2 

77 

78 

124 

143 

13 

14 

57.6 

, 79 

80 

127 

.145 

15 

mm 

59.0 

01 

02 

130 

147 

17 

I® 

60.4 

53 

84 

133 

149 

J9 

20 

61.9 

05 

86 

137 

wnm 

21 

22 

63.4 _ 

07 

88 

_ 140 

153 

23 

24 

64.9 

09 

90 

143 

155 

25 

26 

66.5 

91 

92 

147 

157 

Z7 


20 

60.1 

93 

94 

150 

159 

29 

30 

69.8 

95 

96 

154 .... 

1161 

31 

32 

71.5 

97 : 

9® 

15ft 

i 163 

133 

34: 

73*2 

: 99 

too 

1 162 

165 

35 


36 

75.0 

IOI 

102 

165 

167 

37 \ 


138 

76.8 

103 

104 

169 

169 

39 

- 

40 

78.7 

105 

106 

174 

inni 

4i: 


42 

60,6 

IOI 

108 

! 178 

173 

43 


44 

82.5 

109 

no 

1 182 

175 

45 

46 

84.5 

111 

112 

: 187 

177 

47 

4ft 

86.6 

113 

na 

191 

179 

Esn 

50 

08.7 

\msm 

116 

196 

181 

51 

52 

40.9 

in 

lift 

200 

I&3 

53^ 

54 

93.1 

119 

120 

205 

105 

55. 

T" ' 

56 

95.3 

121 

122 

210 

107 

5T 

50 

97.6 

123 

124 

215 

189 

59 

— 

60 

- too 

125 

126 

221 

191 

6-r 

62 

102 

127 

128 

226 

193 

63 

m 

105 

129 

130 

232 

195 

65 

Gp& 

107 

131 

132 

23 7 

197 


TUe COMPLETE PAPTKJO.15 TWE PU6,U0. 
PLL>8 THE APPLICABLE 'PASU k)0. 


I 


ETinrn i 




DESCRIPTION I DATE I APPRCVAL 


PASH MO 


PESHSTAKJCe 

“OHMS 



134 


136 


130 


140 


142 


144 


146 


i4ft 


ISO 


152 


154 


156 


153 


160 


162 


164 


166 


160 


170 


\iz 


174 


176 


ft 


l&O 


182 


184 


106 


180 


190 


192 


154 


156 


158 


243 


249 


255 


2.01 


201 


274 


200 


ten 


294 


301 


305 


316 


324 


332 


340 


348 


337 


365 


374 


383 


39 2 


402 


412 


422 


432 


442 


433 


464 


475 


487 


495 


511 


523 


215 


217 


219 


221 


223 


225 


227 


229 


23 


233 


235 


237 


239 


241 


243 


245 


247 


245 


251 


253 


255 


257 


759 


261 


263 


too 


tot 


204 


206 


208 


2 


212 


214 


216 


218 


220 


222 


224 


226 


228 


230 


2 32 


234 


236 


238 


240 


242 


244 


246 


248 


250 


252 


254 


256 


258 


260 


261 


204 


349 


562 


576 


59 O 


004 


019 


634 


049 


665 


001 


098 


715 


•732 


1750 


768 


707 


006 


ft25 


045 


666 


687 


909 


931 


953 


976 


IOOO 


1020 


1050 


1070 


noo 


I ISO 


1150 


sovernment/nasa 

NO. 


KOLLSMAN PART NO. 


NOMENCLATURE OR 
DESCRIPTION 


MATERIAL SPECIFICATION 


IB 


| _ LIST OF PARTS AND MATERIALS 

UNLESS OTHERWISE SPECIFIED | ePLh $ u M r A st IWSTRUMEWT CO h P e 0 w R yoSk 


DIMENSIONS ARE IN INCHES | KIC 




MANNED 

SPACECRAFT CENTER 

HOUSTON, TEXAS 


\Z\+ ^ 


W |- ^ I- ^ 1- ^ | 0RAWNXUtkUJJp=OATEi2^ii1 £ g ^>1 STOP Pi X-& D, PlL-M 

DO NOT SCALE THIS DRAWING checked 'jti*<. I--I-6.S - ./.Ai ' 

ATERIAL ipppoval li!) i WviA» l-l'f-if' l/» W . 

see uotes ....... coQTeoi 

A . \ 1 J CODE IDENT NO.I SIZE I NASA NUMBER 


KT ASSY USED ON CONTRACT 

APPLICATION 


LOO no 5: 










































































































































































































































































































































































































I EH BID I 


REVISIONS To** 


DESCRIPTION | DATE I APPROVAL 


*30. |12E5t5TWJ£.E 
OHMS 


1180 


X>A5H MO- 




265 

266 

267 

268 


tv 

215 
215 
277 
21? 
28t 
285 
285 
2S7 
26? 
241 
293 
295 
297 
2*? 9 
30» 
503 
305 
301 
30? 
311 
3l3 
313 
311 
313 
321 
323 
323 
327 
329 


210 

272 

274 

276, 

278 

280 

282 

284 

286 

268 

290 

292 

294 

296 

298 

300 

302 

304 

306 

308 

310 

312 

314 

316 

318 

320 

322 

324 

326 

328 

350 


1240 

1270 

1300 

1330 

1370 

1400 

1430 

1470 

1900 

1540 

1880 

1620 

1650 

1690 

1740 

nao 

1820 

1870 

1310 

1?60 

2000 

2050 

2100 

2150 

2210 

2260 

2320 

2370 

2430 

24?Q 

2550 


IBSB 


331 


333 


335 

337 

339 

341 

343 

343 

347 

549 

351 

353 

355 

357 

355 

361 

363 

365 

367 

369 

371 

313 

315 

371 

319 

3&1 

383 

385 

387 

389 

391 

593 

395 


& 


332 


334 


336 

338 

340 

342 

344 

346 

348 

390 

352 

354 

356 

358 

360 

362 

364 

366 

368 

370 

312 

374 

376 

378 

380 

382 

384 

386 

388 

390 

392 

394 

396 


KE519TAWC6 

OHMS 


2610 


2670 


2740 
2000 
2870 
2940 
I 3010 
; 3Q90 

3160 
3240 
3320 
3400 
3480 
3570 
3650 
3740 
3830 
3920 
4020 
41 20 
4220 
4320 
4420 
4530 
4640 
4750 
4870 
4990 
5110 
5230 
5360 
5490 
5620 


DASH KiO 


lE222S22E3a 

BlI^S 


DASH MO~ 


KGSI3TAWC6 
7 OHMS 


397 


399 


401 

403 

405 

407 

409 

411 

413 

415 

417 

419 

421 

423 

425 

427 

429 

431 

433 

433 

437 

439 

441 

443 

445 

447 

449 

451 

453 

455 

457 

459 

461 


398 


400 


402 

404 

406 

408 

410 

412 

414 

416 

418 

420 

422 

424 

426 

428 

430 

432 

434 

436 

438 

440 

442 

444 

446 

448 

450 

452 

454 

496 

458 

460 

462 


THE COMPLETE PAZT KJO. IS THE PW6 IOO- 
PLUS THE APPLICABLE T?ASM 100. 



57 60 


5900 


6040 
6190 
6340 
6490 
6650 
6810 
6980 
7150 
7320 
7500 
7680 
7870 
8060 
8250 
8450 
8660 
6870 
9090 
9310 
953Q 
9760 
IQ OOP 
10,200 
IQ 300 
10,100 
11, OOP 
11,300 
11, 500 
11,800 
12,100 
12 400 


463 


465 


467 

469 

471 

473 

475 

477 

479 

481 

483 

485 

487 

489 

491 

493 

495 

497 

499 

501 

503 

503 

507 

509 

511 

513 

515 

511 

519 

521 

523 

523 

527 


464 


466 


468 

470 

472 

474 

476 

478 

480 

482 

484 

486 

488 

490 

492 

494 

496 

498 

500 

502 

^04 

506 

508 

510 

312 

814 

516 

518 

520 

522 

524 

326 

528 


I item! qty|.,„ government/nasa 

NO. ptEQcl * * * I NO.' 


13.300 ■ 
13700 
14,000 

14.300 
14, 700 
15,000 

15.400 
15,800 
16, 200 

16.300 

16.900 

17.400 

17.600 
18,200 

18.700 
19, 100 
19, 600 
20,000 
20,500 
21,000 
21, 800 
22100 

22.600 
23,200 
2S, 700 
24 300 

24.900 

25, 500 

26, IOO 

26.700 
<27.400 

KOLLSMAN PART NO. 


NOMENCLATURE OR 
DESCRIPTION 


SPECIFICATION 


LIST OF PARTS AND MATERIALS 


UNLESS OTHERWISE SPECIFIED | ^ S u M H A s W T 1W$TRUMEI,T C0 R n P ° w RA T q°I! 


DIMENSIONS ARE IN INCHES 
I FRACTIONS! DECIMAL! I ANCLES 


Oi38WOO^S 


MANNED 

SPACECRAFT CENTER 

HOUSTON. TEXAS 


°"1- ^ I' ^ I- ^ DSAWN„XL OH kJ 
DO NOT SCALE THIS DRAWING checkeoJ^J-^Lj 

MATERIAL APPROVAl TU) (1 

APPROVAL /S 


NEXT ASSY I USED ON CONTRACT 

APPLICATION 


I NASA APPROVAL. 


I MIT APPROVAL J 


Boater K£SlST0E, f\X£T>, FILM __ 

‘pP&ClPICATlOK) COUTEOL PPAuJlUfc 

A A / CODE IDENT NO.I SIZE NASA NUMBER 

C ioo nos 

SCALE wolji£ weight actual | SMttT 3 of .4~ 

2 1 























































PASM MO. | 

RE315T/MCG’ 

DA.3H MO 




:: ohms 



Hi 

529 

530 


595 

596 

61,900 

531 

532 

28.700 

BBII 

598 

£3,400 

533 

534 


599 

600 


535 

536 

30, IOO 

601 - 

£02 


: 537 

538 

30,900 

EEEB! 


£0, too 

539 

540 

31, 600 

605 

£06 

69,800 

541 

542 

32,400 

607 

608 

71,£00 

543 

544 

33,200 

£09 

610 

73.2OO 

545 

546 

34,000 

611 

612 

75,000 

541 

548 

34,800 

<613 

£14 

76,800 

544 

55 O 

35,700 

£15 


18,100 

551 

552 

36, 500 

617 

£18 

80,600 

.553 

554 

37,400 

619 

£20 

82,500 

555 

556 

38,300 

£21 

£22 

84; 400 

557 _ 

558 

39,2OO 

£23 

£24 

86,600 

559 

560 

40,200 

625 

£2£ 

88, 700 

561 

562 

41,200 

627 

£ 23 

90, 900 

563 

564 

42, 200 

£29 

£30 

93, lOO 

565 

566 

43, 200 

£31 

632 

95,300 

561 

568 

44,200 

£33 

6 34 

97, 600 

569 

57 O 

45, 300 

635 

6 36 

too, 000 

57A 

572 

46, 400 

637 

£38 

102,000 

573 

574 

47, 500 

£39 

640 

105,000 

575 

576 

48,700 

£41 1 

642 

107, OOO 

571 

578 

49,900 

643 ' 

644 

110,000 

519 

580 

51, lOO 

645 

646 

113*000 

581 

582 

52,300 

£47 

648 

115,000 

583 

584 

53, 600 

£49 

6 50 

118,000 

585 

586 

54,900 

651 

6 52 

121,000 

587 

588 

56,200 

653 

6 54 

124,000 

589 

590 

57,600 

655 

656 

127, OOO 

591 

592 

59,000 

657 

658 

130,000 

593 

594 

60,400 

659 

CpCpO 

133,000 


THS COMPLETE PART DO. 1*3 TH£ PW6 Da 
PLUS) THE APPLICABLE pash MO. 




AO-1340 



67i 
£73 
£75 
677 
£7 9 
681 
683 
6e>5 
£87 
689 

69 I 

693 
£97 
699 
7 Ol 
703 

70 & 
707 
703 
7H 
713 
713 
717 
713 
77.1 
773 
713 


672 
674 
676 
£7 a 
680 
682 
684 
£86 
688 
£>30 
£37 
694 
696 
6 98 

700 

707. 

704 

7Q£ 

708 

7 tO 

717 

714 

716 

7 >8 

770 

777 

774 

776 


134,000 
13&.OOQ 
I £7, OOP 
I £3,000 
>£3,000 
17 4,0*00 
118,000 
187,000 

)e>i,ooo 

131,000 
196,000 
700, OOP 
703,000 
710,000 
713,000 
771,000 
726,000 
232,000 
237,000 
243,000 
243,000 
733,000 
261,000 
767,000 
714,000 
280,000 
787,000 
294,000 


777 


729 


731 


733 


735* 


737 

739 

74 > 

743 

743 

741 

749 

731 

733 

793 

7 87 

739 

761 

763 

765 

767 

769 


‘ & 


728 


730 


732 


734 


736 


158 

740 

741 

744 

746 

748 

780 

752 

734 

736 

788 

760 

762 

764 

766 

768 

770 


309,000 


316,000 


324,000 


332,000 


340, 
348000 
337,000 
365,000 
374,000 
333,000 
392,000 
402,000 
412,000 
422,000 
432,000 
442000 
453,000 
464,000 
475,000 
487,000 
499,000 


,TEM QTY sym government/nasa kollsman part no . coot 
NO. REOD * T " NO. »Pg wT 


UNLESS OTHERWISE SPECIFIED RLffJAr >WSTRUMEWT C0 R n P e 0 w R yoSk 

DIMENSIONS ARE IN INCHES KIC A «-» / (V A /"NOv A. 

-1 FRACTIONS I DECIMALS I ANGLeT " ™ 


CODE NOMENCLATURE OR MATERIAL SPECIFICATION 

PART no. idENT DESCRIPTION_ 

LIST OF PARTS AND MATERIALS Z 

STRUMENT CORPORATION MANNED 

- NEW Y0 — spacecraft center 

HOUSTON. TEXAS 


°"1- i- 1- DRAwwTLOHtJtr^DATtiiA^ ^ESISTOI^, PI K&P, Fi LM 

DO WOT SCALE THIS DRAWING checked l-n-OS — • , 

specif I^ATIOO CjQKlTeoluIlgAWuL 

A . A l/t a\ 1 / CODE IDENT NO.I SIZE NASA NUMBER 

...ft-r^ 4 -W « * . 


NEXT ASSY I USED ON CONTRACT 

APPLICATION ___ 

4 4 


I NASA APPROVAL^ 


I MIT APPROVAL. 


| SCALE jJQlJC | WEIGHT 


100 nos 

S8iU I”"" 4- ” 4- 






































































8 


7 


6 


5 


TABLE IT 


REQUIREMENTS: 
i. GENERAL: 

A- INTERPRET DRAWING IN ACCORDANCE 

VJITU STANDARDS PRESCRIBED BY MIL -V-T0Z7 
B- SUPPLIER SHALL COD POEM TO THE QUALIT 
PeOGRAM EEQOIEEMEMTS COMTAIUEDIK) MIL.-0-9S5S 
L. INSPECTION AMD ACCEPTAWCt 

A- MECHANICAL REQUIREMENTS: 

(iJMECUANICAL DIMENSlONSANDTOLERANCe. PtR 
" (Z) LEAD DATA’. LEADS SHALL BE SOLDER ABLE. 
(S)MARKlNG.'(PER MIL-STD-lSO) PARTS SHALL e 
PERMANENTLY AND LEGIBLY MARKED 
WITH THE MANUFACTURERSNAMEORSYMBOI 
TYPE KJO C